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|
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
b6836a475bc534da14ebb8d586a4caa4018c6c67
|
04e4dfecf86c47abbad9ad721bcbc552300a8834
|
/prbs/controller/start.sce
|
08438d540248ca409b3f0c9c9df4840ae5e3837a
|
[] |
no_license
|
rupakrokade/scilab_local_codes
|
702f741a5cadc6da56e428f7379971818238ff22
|
4de8383487def7f18a1f19906397ed4eaf42480e
|
refs/heads/master
| 2021-01-19T06:58:47.689324 | 2015-10-24T11:55:34 | 2015-10-24T11:55:34 | 26,806,574 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 151 |
sce
|
start.sce
|
getd ../../common_files/
getd dc/scilab
exec ../../common_files/loader.sce
exec ser_init.sce
exec prbs_pp.sci
exec twodof_para.sce
xcos prbs_pp.xcos
|
1e6719323269f6cda18d289babc367d8f5039063
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1367/CH4/EX4.4/4_4.sce
|
c6b717cbcf50201d06f466648d7f40551ac65701
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 372 |
sce
|
4_4.sce
|
//Find density of Copper
//Ex:4.4
clc;
clear;
close;
r=1.278;//radius of copper in angstorm
//copper has FCC structure
a=4*r/sqrt(2);//in angstorm
disp(a,"a (in Angstorm) = ");
a1=a*10^-8;//in cm
aw=63.54;//atomic weight of copper
ne=4;//fcc
na=6.023*10^23;//Avagadro's no.
p=aw*ne/(na*a1^3);//in g/cm^3
p1=10^3*p;
disp(p1,"Density of Copper (in kg/cu m)");
|
82303295f5e0c8ead51a393274bf30481b2d00f7
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3754/CH20/EX20.8/20_8.sce
|
1e600703590de5a12b727a3f094a6231028f6c58
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 753 |
sce
|
20_8.sce
|
clear//
//Variables
VS = 24.0 //Source voltage (in volts)
RS = 500.0 //Series resistance (in ohm)
VZ = 12.0 //Zener Voltage (in volts)
IZmin = 3.0 //Minimum Zener current (in milli-Ampere)
IZmax = 90.0 //Maximum Zener current (in milli-Ampere)
rZ = 0.0 //Zener resistance (in ohm)
//Calculation
IS = (VS - VZ) / RS //Current through RS (in Ampere)
ILmax = IS - IZmin * 10**-3 //Maximum value of load Current (in Ampere)
RLmin = VZ / ILmax //Minimum value of Load resistance (in ohm)
//Result
printf("\n Minimum value of load resistance is %0.0f ohm.",RLmin)
|
0d797a0aae52516545ff5719e2109cd2eb3d7e29
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/710/CH13/EX13.4/13_4.sci
|
b3fed4ce4c6f168d6b9ff43affbc384077dbfd32
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 471 |
sci
|
13_4.sci
|
clc();
clear;
//To determine the signal attenuationnper kilometer
pi=100; //mean optical power launched in micro meter
po=5; //mean optical power at fibre output
S=10*log10(pi/po); //signal attenuation un dB
l=6; //length in km
Sk=S/l //signal ayyenuation per kilometer
printf("The signal attenuation per kilometer is %f dB/km",Sk);
|
5d982460ee563ab043eb7526df0dc4d118870691
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3888/CH4/EX4.3/Ex4_3.sce
|
029f1c278ab71b451be24b8b8b824087a5674489
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,428 |
sce
|
Ex4_3.sce
|
//Electric Power Generation, Transmission and Distribution by S.N.Singh
//Publisher:PHI Learning Private Limited
//Year: 2012 ; Edition - 2
//Example 4.3
//Scilab Version : 6.0.0 ; OS : Windows
clc;
clear;
peak_dem_light=200; //Peak demand of the light load in kW
max_dem_light=200; //Maximum demand of the light load in kW
max_dem_rest=1800; //Maximum demand of the rest load in kW
peak_dem_rest=1800; //Peak demand of the rest load in kW
c_light=peak_dem_light/max_dem_light; //Contribution factor for street lighting load
c_rest=peak_dem_rest/max_dem_rest; //Contribution factor for street rest load
DF=(peak_dem_light+peak_dem_rest)/(c_light*max_dem_light+c_rest*max_dem_rest); //Diversity factor of the feeder
CF=1/DF; //Coincidence factor of the load group
printf("\nClass contribution factor for street lightning is %.1f and the remaining load is %.1f",c_light,c_rest);
printf("\nDiversity factor of the feeder %.1f",DF);
printf("\nCoincidence factor of the load group %.1f",CF);
|
e58ae7c6d9dd97e1fa9ca12cc1d321c3dd49e7a0
|
8217f7986187902617ad1bf89cb789618a90dd0a
|
/source/2.0/macros/tdcs/obs_cont.sci
|
498db57e97e4109d733d7ad61d9e9316ac443942
|
[
"MIT",
"LicenseRef-scancode-public-domain",
"LicenseRef-scancode-warranty-disclaimer"
] |
permissive
|
clg55/Scilab-Workbench
|
4ebc01d2daea5026ad07fbfc53e16d4b29179502
|
9f8fd29c7f2a98100fa9aed8b58f6768d24a1875
|
refs/heads/master
| 2023-05-31T04:06:22.931111 | 2022-09-13T14:41:51 | 2022-09-13T14:41:51 | 258,270,193 | 0 | 1 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,094 |
sci
|
obs_cont.sci
|
//[macr]=obs_cont(sysn)
//[macr]=obs_cont(sysn)
//
//cette macro renvoit le systeme observe-commande
//construit a partir du systeme sysn linearise autour de (xe,ue)
//
// sysn : chaine de caractere donnant le nom du systeme a commander
// gaincom,gainobs : vecteurs colonnes des gains demandes
//
// Retour : une nouvelle macro donnant le syst\`eme observe-commande
// [x1dot]=macr(t,x1,abruit,pas,n)
// x1=[x;xchap],
// pour l'appel il faudra creer un vecteur de bruit de nom br
// d'autre part la macro cr\'ee va chercher dans l'environnement
// global les valeurs de (xe,ue) le point d'equilibre
// f,g,h les matrices du systeme linearise
// l et k les deux matrices de gain
// exemple :
// pas=10;n=200;
// br=rand(1,n)
// ode([x0;xchap0],0,pas*(0:n),list(macr,1.0,pas,n));
//!
deff('[zdot]=macr(t,z,abr,pas,n)',...
['u=ue-k(1)*(z(3)-xe(1))-k(2)*(z(4)-xe(2))';
'ff_brui=abr*br(ent(mini(t/pas+1,n)))';
'y=h(1)*z(1)+h(2)*z(2)+ff_brui';
'xdot='+sysn+'(t,z(1:2),u)';
'xdot1=f*(z(3:4)-xe) +g*(u-ue)-l*(h*z(3:4)-y)';
'zdot=[xdot;xdot1]';]);
//end
|
b9058bfdf94d0e07fdf49d5ef3d9c43eb5f237ed
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/551/CH5/EX5.27/27.sce
|
463bd18bc2d431097eb511e4c03a7f7469900604
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 338 |
sce
|
27.sce
|
clc
p1=7*10^5; //N/m^2
T1=873; //K
p2=1.05*10^5; //N/M62
n=1.25;
m=1; //kg
R=0.287;
cp=1.005;
T2=T1*(p2/p1)^((n-1)/n);
// At constant temperature from 1 to A
ds_1A=R*log(p1/p2);
// At constant pressure from A to 2
ds_2A=cp*log(T1/T2);
ds_12=ds_1A - ds_2A;
disp("Increase in entropy = ")
disp(ds_12)
disp("kJ/kg.K")
|
e642e4a7bd043672b9d0da593513db50b315153a
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2063/CH8/EX8.4/8_4.sce
|
e1990333e6df71d3464c33988abe84c619cb5aa2
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,141 |
sce
|
8_4.sce
|
clc
clear
//Input data
P1=10;//Pressure of steam in bar
f=0.9;//Dryness fraction of steam
At=350;//Throat area in mm^2
Pb=1.4;//Back pressure in bar
h1=2574.8;//Enthalpy of steam at nozzle inlet from steam tables in kJ/kg
ft=0.87;//Dryness fraction of steam at throat pressure
fe=0.81;//Dryness fraction of steam at exit pressure
ht=2481;//Enthalpy of steam at throat pressure at ft in kJ/kg
vt=0.285;//Specific volume of steam at throat in m^3/kg
he=2266.2;//Enthalpy of steam at exit conditions in kJ/kg
ve=1.001;//Specific volume of steam at exit conditions in m^3/kg
//Calculations
Pt=0.582*P1;//Steam pressure at the throat in bar
hd=h1-ht;//Enthalpy drop upto the throat in kJ/kg
Vt=44.7*(hd)^(0.5);//Velocity of steam at the throat in m/s
hde=h1-he;//Enthalpy drop from nozzle entrance to exit in kJ/kg
Ve=44.7*(hde)^(0.5);//Velocity of steam at nozzle exit in m/s
Ae=(At*Vt*ve)/(Ve*vt);//Exit area of nozzle from the mass rate of flow equation in mm^2
//Output
printf('(a)Final exit velocity of steam is %3.1f m/s\n (b)Cross sectional area of the nozzle at exit for maximum discharge is %3.0f mm^2',Ve,Ae)
|
e29bf11c234e577775131bd73bff0f0283c932fb
|
9ad712cefe61d85b01d2448a5b74c34296ee7e5f
|
/LAB1.sce
|
f987acc16a18d93d103c8b70ff0065e7ffacfba9
|
[] |
no_license
|
CoE-Warintorn/Control
|
a50f7cf26d0e80e3b90ea9dc3cac097b67f94d49
|
9572040e0e41d8d355f51032cd2ac98b1d04db64
|
refs/heads/master
| 2020-03-16T06:56:11.148006 | 2018-05-08T07:02:35 | 2018-05-08T07:02:35 | 132,565,771 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 693 |
sce
|
LAB1.sce
|
s = poly(0, 's');
t = 0:0.01:10;
Km = 10^-3;
Kb = 5.5*10^-2;
La = 10*10^-6;
Ra = 0.2;
Jm = 1*10^-3;
Dm = 1*10^-2;
//Gs = Km/((La*s + Ra)*(Jm*s^2 + Dm*s) + Km*Kb*s)
Gs = Km/((Ra)*(Jm*s^2 + Dm*s) + Km*Kb*s)
Gs1 = syslin('c', Gs);
Ts = Gs1/(1+Gs1);
den1 = denom(Ts);
routh_t(den1);
//plot(t,csim('step', t, Ts))
Wn = sqrt(5);
Theta = 10.275/(2*Wn);
Theta1 = -log(0.1)/sqrt(%pi^2 + log(0.1)^2)
Theta2 = -log(0.2)/sqrt(%pi^2 + log(0.2)^2)
evans(Gs1)
sgrid([Theta1,Theta2],1)
K = 2055
K1 = 15.1
K2 = 25.43
Ts = K*Gs1/(1+K*Gs1)
Ts1 = K1*Gs1/(1+K1*Gs1)
Ts2 = K2*Gs1/(1+K2*Gs1)
//plot(t,csim('step', t, Ts),t,csim('step', t, Ts1),t,csim('step', t, Ts2))
xgrid()
|
55a2de451dfba63490d085b61a59841b7e41f397
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2774/CH4/EX4.9/Ex4_9.sce
|
da60348d9c3cb44d49bb2004b6003d614d10534d
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 556 |
sce
|
Ex4_9.sce
|
clc
// initialization of variables
V1=2 // initial volume in m^3
V2=0.2 // final volume in m^3
T1=20+273// temperature in kelvin
P=200 // pressure in kPa
R=0.287 // constant for air
gama=1.4 // polytropic index for air
Cv=0.717// specific heat at constant volume for air
//solution
//using the ideal gas equation
m=(P*V1)/(R*T1) // mass in kg
// process is adiabatic thus
T2=T1*((V1/V2)**(gama-1))// final temperature
W=-m*Cv*(T2-T1)// work from first law
printf("The Work is "+string(W)+" kJ")
// solution is approximated in textbook
|
33988a1650a09d900fe60974c5e80ccac53d8c75
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/55/CH12/EX12.4/12ex4.sci
|
8b834b24ad185aabee3e8a9e3a23949702007a33
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 375 |
sci
|
12ex4.sci
|
a=(8-4)-3
b=8-(4-3)
disp('since a and b are not equal so subtraction is non-commutative on Z(set of integers)')
a=[1 2;3 4]
b=[5 6;0 -2]
g= a*b
k= b*a
disp('since g and k are not equal matrix multiplication is non-commutative')
h=(2^2)^3
j=2^(2^3)
disp('since h and j are not equal so exponential operation is non associative on the set of positive integers N')
|
2e5da7a0e1d73da4b5ec7a3a958b68b00a6021c1
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2747/CH1/EX1.1/Ex1_1.sce
|
e0cf3f3b686815173ee2ea0e784b56d919d859ee
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 180 |
sce
|
Ex1_1.sce
|
clc
clear
//Initialization of variables
gc=32.1739 //lbm ft/lbf s^2
m=10 //lbm
a=10 //ft/s^2
//calculations
F=m*a/gc
//results
printf("Force to accelerate = %.3f lbf",F)
|
2b50ccc6fcc6cda1a020a22d572efd78df9419bd
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1664/CH2/EX2.2/Ex2_2.sce
|
d686a93f7f6eb9e738b72534b1427854da2fa307
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 357 |
sce
|
Ex2_2.sce
|
//Example No.2.2.
// Page No.60.
clc;clear;
w = 632.8*10^(-9);//wavelength -[m].
h = 6.626*10^(-34);//Planck's constant.
c = (3*10^(8));//Velocity of light.
E = ((h*c)/(w));// Energy of one photon
printf("\nThe energy of emitted photon in joules is %3.3e J",E);
E = E/(1.6*10^(-19));
printf("\nThe energy of emitted photon in eV is %.2f eV",E);
|
f0b77dede391da08a0e48482bbd39376f9a846ee
|
b29e9715ab76b6f89609c32edd36f81a0dcf6a39
|
/ketpic2escifiles6/Viewfrom.sci
|
44bde517afc579ce11f93026c55ca7df2dea5254
|
[] |
no_license
|
ketpic/ketcindy-scilab-support
|
e1646488aa840f86c198818ea518c24a66b71f81
|
3df21192d25809ce980cd036a5ef9f97b53aa918
|
refs/heads/master
| 2021-05-11T11:40:49.725978 | 2018-01-16T14:02:21 | 2018-01-16T14:02:21 | 117,643,554 | 1 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 358 |
sci
|
Viewfrom.sci
|
// 08.10.26
function Out=Viewfrom(varargin)
global THETA PHI
Nargs=length(varargin);
Nvec=varargin(1);
GL=varargin(2);
Flg=1;
if Nargs>=3
Flg=varargin(3);
end;
Theta=THETA; Phi=PHI;
Tmp=Rotate3data(GL,Nvec,[-1,0,0]);
THETA=%pi/2; PHI=0;
Out=Projpara(Tmp);
if Flg==1
Windisp(Out);
end;
THETA=Theta; PHI=Phi;
endfunction;
|
51cd7423740c6a031b45dee1e8cd213539fabdfb
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/608/CH23/EX23.01/23_01.sce
|
0bf483fa0148f5158d881ece82c45bbdfbdcab05
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 449 |
sce
|
23_01.sce
|
//Problem 23.01: In an electrical circuit the total impedance ZT is given by ZT = (Z1*Z2/(Z1 + Z2))+ Z3. Determine ZT in (a + jb) form, correct to two decimal places, when Z1 = 5 - j3, Z2 = 4 - i7 and Z3 = 3.9 - i6.7.
//initializing the variables:
Z1 = 5 - 3*%i;
Z2 = 4 + 7*%i;
Z3 = 3.9 - 6.7*%i;
//calculation:
ZT = (Z1*Z2/(Z1 + Z2))+ Z3
y = imag(ZT)
x = real(ZT)
printf("\n\n Result \n\n")
printf("\n ZT is %.2f + (%.2f)i", x,y)
|
5827ef8860c8e52ee5296a075aee20e472050f21
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1445/CH7/EX7.28/ch7_ex_28.sce
|
8d9b3185f768ab52e7bf38e9fed2c673d065b9a1
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 2,604 |
sce
|
ch7_ex_28.sce
|
//CHAPTER 7- SINGLE PHASE TRANSFORMER
//Example 28
disp("CHAPTER 7");
disp("EXAMPLE 28");
//VARIABLE INITIALIZATION
va=10000; //apparent power
v1=2500; //primary voltage in Volts
v2=250; //secondary voltage in Volts
f=50;
//open circuit parameters
Voc=250;
Io=0.8;
Wi=50; // watts HT side
//short circuit test
Vsc=60;
Isc=3;
Wc=45; // watts HT side
//
//loads
pf=0.8;
//SOLUTION
I1=va/v1; //full rated current on hv side
Psc0=Wc*(I1/Isc)^2; //ohmic loss/ cu loss at full load rated current
Pc=Wi; // core losses
// 1/4 load
Psc=(1/4)^2*Psc0;
Pout=va*pf*(1/4);
Pin=Pout+Pc+Psc;
eff=Pout*100/Pin;
disp("SOLUTION (a)");
disp(sprintf("The efficiency at 1/4 load is %f",eff));
//
// 1/2 load
Psc=(1/2)^2*Psc0;
Pout=va*pf*(1/2);
Pin=Pout+Pc+Psc;
eff=Pout*100/Pin;
disp(sprintf("The efficiency at 1/2 load is %f",eff));
//
// full load
Psc=(1/1)^2*Psc0;
Pout=va*pf*(1/1);
Pin=Pout+Pc+Psc;
eff=Pout*100/Pin;
disp(sprintf("The efficiency at full load is %f",eff));
//
// 1 1/4 = 5/4 load
Psc=(5/4)^2*Psc0;
Pout=va*pf*(5/4);
Pin=Pout+Pc+Psc;
eff=Pout*100/Pin;
disp(sprintf("The efficiency at 1 1/4 or 5/4 load is %f",eff));
//
//maximum efficiency at x, but then ohmic loss=core loss
x=sqrt(Pc/Psc0);
Pout=va*x*pf;
Pin=Pout+Pc+Pc; //Ohmic losses = core losses at max efficiency
eff=Pout*100/Pin;
disp("SOLUTION (b)");
disp(sprintf("The maximum efficiency is %f",eff));
//
//short circuit
phisc=acos(Wc/(Vsc*Isc));
pf1=cos(phisc);
R_e1=Vsc*pf1/Isc;
Z_e1=Vsc/Isc;
X_e1=sqrt(Z_e1^2-R_e1^2);
disp("SOLUTION (c)");
disp(sprintf("The value of Re1 is %f Ohm",R_e1));
disp(sprintf("The value of Ze1 is %f Ohm",Z_e1));
disp(sprintf("The value of Xe1 is %fΩ",X_e1));
//
//ee, ex;
er=I1*R_e1/v1;
ex=I1*X_e1/v1;
disp(sprintf("The value of Er is %f pu",er));
disp(sprintf("The value of Ex is %f",ex));
//
phi=acos(pf);
//R=ercosphi2+vx.sinphi2
//E2=V2+I2.R
%reg=(I1*R_e1*pf+I1*X_e1*sin(phi))*100/v1; //same as using er and ex
disp(sprintf("The percent regulation at full load lagging is %f",%reg));
%reg1=(I1*R_e1*pf-I1*X_e1*sin(phi))*100/v1; //same as using er and ex
disp(sprintf("The percent regulation at full load leading is %f",%reg1));
V21=(1-%reg/100)*v2;
V22=(1-%reg1/100)*v2;
disp(sprintf("The secondary terminal voltage at full load lagging is %f",V21));
disp(sprintf("The secondary terminal voltage at full load leading is %f",V22));
disp(" ");
//
//END
|
e2a04ad45efcb949e44535f2da8ca5048ab294e9
|
a62e0da056102916ac0fe63d8475e3c4114f86b1
|
/set12/s_Higher_Engineering_Mathematics_B._S._Grewal_149.zip/Higher_Engineering_Mathematics_B._S._Grewal_149/CH10/EX10.13/ques13.sce
|
520cc283034c1dc18c15fbe289693ab794a2f026
|
[] |
no_license
|
hohiroki/Scilab_TBC
|
cb11e171e47a6cf15dad6594726c14443b23d512
|
98e421ab71b2e8be0c70d67cca3ecb53eeef1df6
|
refs/heads/master
| 2021-01-18T02:07:29.200029 | 2016-04-29T07:01:39 | 2016-04-29T07:01:39 | null | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 279 |
sce
|
ques13.sce
|
errcatch(-1,"stop");mode(2);//ques13
disp('The complex form of series is summation of f(n,x) where n varies from -%inf to %inf and f(n,x) is given by :');
syms n x
cn=1/2*integ(exp(-x)*exp(-%i*%pi*n*x),x,-1,1);
fnx=float(cn)*exp(%i*n*%pi*x);
disp(float(fnx));
exit();
|
bf43d7609eef92d92be69a518afe3b7d828d3fc4
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1928/CH1/EX1.5.1/ex1_5_1.sce
|
df87ea9c0adec7d636af212b2bd338b7db9336e0
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 483 |
sce
|
ex1_5_1.sce
|
//Chapter-1,Example1_5_1,pg 1-29
//refer diagram from textbook
//on joining centre of 3 anions,an equilateral triangle is formed and on joining centres of any anion and cation a right angle triangle ABC os formed
//where AC=rc+ra
//and BC=ra
//m(angle (ACB))=30 degree
//therefore cos (30)=ra/(rc+ra)
//assume rc/ra=r
r=(1-cosd(30))/cosd(30) //by arrangimg terms we get value of r
printf("critical radius ratio of ligancy 3=")
disp(r)
|
0b72a37a363a8ac39603acfa050d78ea0a0ce5e7
|
51635684d03e47ebad12b8872ff469b83f36aa52
|
/external/gcc-12.1.0/gcc/testsuite/ada/acats/tests/cd/cd4041a.tst
|
d0e2fd65d6a2b193fb43209b4f21f06c848c1d1d
|
[
"Zlib",
"LicenseRef-scancode-public-domain",
"LGPL-2.1-only",
"FSFAP",
"LGPL-3.0-only",
"GPL-3.0-only",
"GPL-2.0-only",
"GCC-exception-3.1",
"LGPL-2.0-or-later"
] |
permissive
|
zhmu/ananas
|
8fb48ddfe3582f85ff39184fc7a3c58725fe731a
|
30850c1639f03bccbfb2f2b03361792cc8fae52e
|
refs/heads/master
| 2022-06-25T10:44:46.256604 | 2022-06-12T17:04:40 | 2022-06-12T17:04:40 | 30,108,381 | 59 | 8 |
Zlib
| 2021-09-26T17:30:30 | 2015-01-31T09:44:33 |
C
|
UTF-8
|
Scilab
| false | false | 3,363 |
tst
|
cd4041a.tst
|
-- CD4041A.TST
-- Grant of Unlimited Rights
--
-- Under contracts F33600-87-D-0337, F33600-84-D-0280, MDA903-79-C-0687,
-- F08630-91-C-0015, and DCA100-97-D-0025, the U.S. Government obtained
-- unlimited rights in the software and documentation contained herein.
-- Unlimited rights are defined in DFAR 252.227-7013(a)(19). By making
-- this public release, the Government intends to confer upon all
-- recipients unlimited rights equal to those held by the Government.
-- These rights include rights to use, duplicate, release or disclose the
-- released technical data and computer software in whole or in part, in
-- any manner and for any purpose whatsoever, and to have or permit others
-- to do so.
--
-- DISCLAIMER
--
-- ALL MATERIALS OR INFORMATION HEREIN RELEASED, MADE AVAILABLE OR
-- DISCLOSED ARE AS IS. THE GOVERNMENT MAKES NO EXPRESS OR IMPLIED
-- WARRANTY AS TO ANY MATTER WHATSOEVER, INCLUDING THE CONDITIONS OF THE
-- SOFTWARE, DOCUMENTATION OR OTHER INFORMATION RELEASED, MADE AVAILABLE
-- OR DISCLOSED, OR THE OWNERSHIP, MERCHANTABILITY, OR FITNESS FOR A
-- PARTICULAR PURPOSE OF SAID MATERIAL.
--*
-- OBJECTIVE:
-- CHECK THAT AN ALIGNMENT CLAUSE CAN BE GIVEN FOR A RECORD
-- REPRESENTATION CLAUSE.
-- HISTORY:
-- RJW 08/25/87 CREATED ORIGINAL TEST.
-- DHH 03/30/89 CHANGED MOD 4 TO A MACRO VALUE AND CHANGED
-- EXTENSION FROM '.DEP' TO '.TST'.
-- MACRO SUBSTITUTION:
-- $ALIGNMENT IS THE VALUE USED TO ALIGN A RECORD ON A BOUNDARY
-- DEFINED BY THE IMPLEMENTATION.
WITH REPORT; USE REPORT;
WITH SYSTEM;
PROCEDURE CD4041A IS
UNITS_PER_INTEGER : CONSTANT :=
(INTEGER'SIZE + SYSTEM.STORAGE_UNIT - 1) /
SYSTEM.STORAGE_UNIT;
TYPE CHECK_CLAUSE IS RECORD
INT_COMP : INTEGER;
CHAR_COMP : CHARACTER;
END RECORD;
FOR CHECK_CLAUSE USE
RECORD AT MOD $ALIGNMENT;
INT_COMP AT 0
RANGE 0..INTEGER'SIZE - 1;
CHAR_COMP AT 1*UNITS_PER_INTEGER
RANGE 0..CHARACTER'SIZE - 1;
END RECORD;
CHECK_RECORD : CHECK_CLAUSE := (1, 'A');
BEGIN
TEST ("CD4041A", "CHECK THAT AN ALIGNMENT CLAUSE CAN BE " &
"GIVEN FOR A RECORD REPRESENTATION CLAUSE");
IF CHECK_RECORD.INT_COMP'FIRST_BIT /= 0 THEN
FAILED ("INCORRECT VALUE FOR FIRST_BIT OF INT_COMP");
END IF;
IF CHECK_RECORD.INT_COMP'LAST_BIT /= INTEGER'SIZE - 1 THEN
FAILED ("INCORRECT VALUE FOR LAST_BIT OF INT_COMP");
END IF;
IF CHECK_RECORD.INT_COMP'POSITION /= 0 THEN
FAILED ("INCORRECT VALUE FOR POSITION OF INT_COMP");
END IF;
IF CHECK_RECORD.CHAR_COMP'FIRST_BIT /= IDENT_INT (0) THEN
FAILED ("INCORRECT VALUE FOR FIRST_BIT OF CHAR_COMP");
END IF;
IF CHECK_RECORD.CHAR_COMP'LAST_BIT /=
IDENT_INT (CHARACTER'SIZE - 1) THEN
FAILED ("INCORRECT VALUE FOR LAST_BIT OF CHAR_COMP");
END IF;
IF CHECK_RECORD.CHAR_COMP'POSITION /=
IDENT_INT (UNITS_PER_INTEGER) THEN
FAILED ("INCORRECT VALUE FOR POSITION OF CHAR_COMP");
END IF;
RESULT;
END CD4041A;
|
09652540233fd3700ee5ae71068967cd3bac5614
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2609/CH5/EX5.14/ex_5_14.sce
|
2a70b2f0322e5d4723dba09e07721c7ea65aadcc
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 238 |
sce
|
ex_5_14.sce
|
//Ex 5.14
clc;
clear;
close;
format('v',4);
R1=1;//kohm
R2=1;//kohm
R3=1;//kohm
Rf=R2+R3;//kohm
Vin=1;//V
//Capacitor remains open circuited for steady state in both cases.
Vout=-Rf/R1*Vin;//V
disp(Vout,"Output Voltage(V)");
|
b9ab10f40f8b50377fa38367c5c46d3a3ea80afb
|
3c47dba28e5d43bda9b77dca3b741855c25d4802
|
/microdaq/macros/mdaq_exec_profile.sci
|
56bbe1b82fd584b25fcbeb3c902806edf930b2d2
|
[
"BSD-3-Clause"
] |
permissive
|
microdaq/Scilab
|
78dd3b4a891e39ec20ebc4e9b77572fd12c90947
|
ce0baa6e6a1b56347c2fda5583fb1ccdb120afaf
|
refs/heads/master
| 2021-09-29T11:55:21.963637 | 2019-10-18T09:47:29 | 2019-10-18T09:47:29 | 35,049,912 | 6 | 3 |
BSD-3-Clause
| 2019-10-18T09:47:30 | 2015-05-04T17:48:48 |
Scilab
|
UTF-8
|
Scilab
| false | false | 370 |
sci
|
mdaq_exec_profile.sci
|
function data = mdaq_exec_profile()
data = [];
if isfile(TMPDIR + filesep() + "profiling_data") then
load(TMPDIR + filesep() + "profiling_data");
data = dsp_exec_profile;
clear dsp_exec_profile;
else
disp("WARNING: Unable to get profiling data - make sure it is enabled in SETUP block!")
return;
end
endfunction
|
0fac87c1915b79001547f2265ae648654a6ff7d6
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3878/CH21/EX21.2/Ex21_2.sce
|
67587f834a78520d05b43da51805d4e2e6b174cd
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 383 |
sce
|
Ex21_2.sce
|
clear
// Variable declaration
Q=500// The amount of heat required for the building in kW
T=19// The temperature at which air enters the heater coil in °C
m_a=68// // The mass flow rate of air in kg/s
C_pa=1.02// The specific heat capacity of air in kJ/kg.K
// Calculation
t=T+(Q/(m_a*C_pa))// The air supply temperature in °C
printf("\n The air-supply temperature,t=%2.1f°C",t)
|
5d37c1d7a7a118a517440fb611079e8cdb50fc68
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1163/CH6/EX6.8/example_6_8.sce
|
d951ece5a4524a7ac184749990cf4a00f0332758
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,916 |
sce
|
example_6_8.sce
|
clear;
clc;
disp("--------------Example 6.8---------------")
n=4; // number of channels
channel_byte=1; // each frame carries 1 byte from each channel
frame_size=n*channel_byte; //bytes
frame_size_bits=frame_size*8; // 1 byte = 8 bits
byte_rate=100; // each channel sends 100 bytes/s
frame_rate=channel_byte*byte_rate; // frames per second
frame_duration=1/frame_rate; // seconds
bit_rate=frame_rate*frame_size_bits; // bps
// display the result
printf("Each frame carries %d byte from each channel; the size of each frame, therefore, is %d bytes, or %d bits.\nThe frame rate is %d frames per second. The duration of a frame is %3.2f s.\nThe bit rate is %d bps.",channel_byte,frame_size,frame_size_bits,frame_rate,frame_duration,bit_rate);
// display the figure
clf();
xname("--------------Example 6.8----------------");
xpoly([.3 .3],[.3 .7]);
xset("color",4.2);
xfrect(0,.7,.28,.05);
xfrect(.58,.58,.035,.045);
xfrect(.88,.58,.035,.045);
xset("color",2.9);
xfrect(0,.6,.28,.05);
xfrect(.545,.58,.035,.045);
xfrect(.845,.58,.035,.045);
xset("color",3.8);
xfrect(0,.5,.28,.05);
xfrect(.51,.58,.035,.045);
xfrect(.81,.58,.035,.045);
xset("color",0);
xfrect(0,.4,.28,.05);
xfrect(.475,.58,.035,.045);
xfrect(.775,.58,.035,.045);
xpoly([-.05 .3],[.625 .625]);
xpoly([-.05 .3],[.525 .525]);
xpoly([-.05 .3],[.425 .425]);
xpoly([-.05 .3],[.325 .325]);
xset("font size",4)
xstring(.33,.5,"MUX");
xpoly([.3 .45],[.7 .5]);
xpoly([.3 .45],[.3 .5]);
xstring(.1,.27,"100 bytes/s");
xset("font size",3)
xstring(.65,.45,"100 frames/s");
xstring(.67,.41,"3200 bps");
xstring(.6,.33,"Frame duration = 1/100 s");
xstring(.5,.7,"Frame 4 bytes");
xstring(.8,.7,"Frame 4 bytes");
xstring(.54,.65,"32 bits");
xstring(.84,.65,"32 bits");
xrect(.47,.59,.15,.07);
xrect(.77,.59,.15,.07);
xset("thickness",2);
xarrows([.45 1],[.5 .5],.2);
xset("font size",7);
xstring(.66,.53,". . .");
|
c2ec84e16f3ff009c2ddfc557178d756a98e1ec3
|
48d313982e11468e3406524c01f1cba2700a2db5
|
/Calcul numeric/ResurseTemaCalculNumeric/New folder/Mcmp/LevenbergMarquardt/f1.sce
|
30d1325fc5bce19005b5ac17a41dc914ae585039
|
[] |
no_license
|
albanionut/University
|
b8e918a192c131647099c57e1b2caa231de98d6d
|
b3d3dfe3cf64d0cddfaeb570151adf7d4c9ad0b7
|
refs/heads/master
| 2021-07-13T11:31:29.880681 | 2020-10-10T15:07:00 | 2020-10-10T15:07:00 | 214,223,943 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 58 |
sce
|
f1.sce
|
function y=f1(x,t)
y=x(1)*exp(x(2)*t);
endfunction
|
7a9a599d4cd6624e80adfa7d32bbb5099af5ee9d
|
8ea401b354e99fe129b2961e8ee6f780dedb12bd
|
/macros/combine.sci
|
52794630010715056b20142acff71a43497f6634
|
[
"BSD-2-Clause"
] |
permissive
|
adityadhinavahi/SciPandas
|
91340ca30e7b4a0d76102a6622c97733a28923eb
|
b78b7571652acf527f877d9f1ce18115f327fa18
|
refs/heads/master
| 2022-12-20T04:04:35.984747 | 2020-08-19T16:10:51 | 2020-08-19T16:10:51 | 288,765,541 | 0 | 1 | null | 2020-08-19T15:35:04 | 2020-08-19T15:14:46 |
Python
|
UTF-8
|
Scilab
| false | false | 797 |
sci
|
combine.sci
|
function combine()
// Perform column-wise combine with another DataFrame.
//
// Syntax
// dfr.combine(obj,input_string)
//
// Parameters
// obj : DataFrame object
// input_string : String containing the function to be passed. Scilab functions are not supported as of now. Additional parameters supported can be passed
// // For additional information on parameters, see https://pandas.pydata.org/docs/reference/api/pandas.DataFrame.combine.html?#pandas.DataFrame.combine
// Returns : DataFrame
//
// Examples
// // Combine another DataFrame with this DataFrame by using np.sqrt function
// dfr.combine(df1.age,"np.sqrt") //
// // Lambda functions are also supported.
//
// Authors
// Aditya Dhinavahi
// Sundeep Akella
endfunction
|
1d6fe4d54af9f60ed4dae8078981c43b5424d62b
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/32/CH12/EX12.05/12_05.sce
|
dba2676402bea1e854d9f14fe1bdc1f7dd3fff5d
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 894 |
sce
|
12_05.sce
|
//pathname=get_absolute_file_path('12.05.sce')
//filename=pathname+filesep()+'12.05-data.sci'
//exec(filename)
//Steam consumption rate(in kg/a):
m=18/60
//Indicated power(in kW):
IP=100
//Rpm of engine:
n=240
//Bore diameter(in m):
d=0.3
//Stroke length(in m):
L=0.4
//Pressure at which steam is admitted(in bar):
p1=10
//Exhaust pressure(in bar):
p3=0.75
//Occurance of cut-off:
r1=0.25
//Enthalpy of steam(in kJ/kg):
h1=2875.3 //kJ/kg
hf=384.39 //kJ/kg
//Heat added per kg of steam(in kJ/kg):
Q=h1-hf
//Expansion ratio:
r=1/r1
//Hypothetical mean effective pressure(in bar):
mep=p1/r*(1+log(r))-p3
//Theoretical indicated power(in kW):
IPt=mep*L*%pi*d^2*n*10^2/(60)
//Diagarm factor:
d1=IP/IPt
//Indicated thermal efficiency:
n=IPt/(m*Q)*100
printf("\n RESULT \n")
printf("\nDiagram factor = %f",d1)
printf("\nIndicated thermal efficiency = %f percent",n)
|
6e54dbbde045cfd26782185b97a27cb6ff0fad2a
|
4a1effb7ec08302914dbd9c5e560c61936c1bb99
|
/Project 2/Experiments/FURIA-C/results/FURIA-C.vowel-10-1tra/result4s0.tst
|
100b05c06cd7ea6e5d352b9704f76e0aca4f8b75
|
[] |
no_license
|
nickgreenquist/Intro_To_Intelligent_Systems
|
964cad20de7099b8e5808ddee199e3e3343cf7d5
|
7ad43577b3cbbc0b620740205a14c406d96a2517
|
refs/heads/master
| 2021-01-20T13:23:23.931062 | 2017-05-04T20:08:05 | 2017-05-04T20:08:05 | 90,484,366 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 983 |
tst
|
result4s0.tst
|
@relation vowel
@attribute TT integer[0,1]
@attribute SpeakerNumber integer[0,14]
@attribute Sex integer[0,1]
@attribute F0 real[-5.211,-0.941]
@attribute F1 real[-1.274,5.074]
@attribute F2 real[-2.487,1.431]
@attribute F3 real[-1.409,2.377]
@attribute F4 real[-2.127,1.831]
@attribute F5 real[-0.836,2.327]
@attribute F6 real[-1.537,1.403]
@attribute F7 real[-1.293,2.039]
@attribute F8 real[-1.613,1.309]
@attribute F9 real[-1.68,1.396]
@attribute Class{0,1,2,3,4,5,6,7,8,9,10}
@inputs TT,SpeakerNumber,Sex,F0,F1,F2,F3,F4,F5,F6,F7,F8,F9
@outputs Class
@data
0 0
4 4
6 8
1 1
7 8
8 8
0 0
1 1
2 1
1 1
6 9
5 5
1 1
4 4
6 10
6 10
10 10
3 3
8 8
10 10
1 1
2 2
3 3
5 5
10 10
6 6
7 7
10 10
3 3
6 6
0 0
1 0
9 9
7 7
1 1
5 5
2 2
0 0
1 1
6 6
3 10
0 0
2 2
7 9
9 9
10 10
3 3
5 4
3 3
4 4
7 7
2 2
7 7
8 6
0 0
7 7
9 9
8 9
8 9
9 9
4 4
8 9
10 10
9 9
2 2
5 10
3 3
0 1
8 8
3 3
5 4
8 8
0 1
2 1
6 6
7 7
4 4
5 5
9 9
1 1
2 10
10 10
9 9
4 4
4 4
9 9
10 10
8 8
4 4
4 4
9 9
0 0
7 7
5 10
10 10
2 10
3 3
5 5
6 6
|
1b585808baae60be7e55c651d8c51e16ca14acbc
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/29/CH6/EX6.10.5/exa6_10_5.sce
|
34107206db6e4243a0599c78a6ecad88afb6a8e0
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,015 |
sce
|
exa6_10_5.sce
|
//Caption:calculate_Wn,zeta,Wd,tp,Mp
//example 6.10.5
//page 174
//given G(s)=20/(s+1)*(s+2)
clc;
s=%s;
G=syslin('c',[20/((s+1)*(s+5))])//G(s):transfer function in forward path
H=1;//backward path transfer function
a=G/.H //closed loop transfer function
b=denom(a)
c=coeff(b)
//Wn^2=c(1,1)
Wn=sqrt(c(1,1))//natural frequency
disp(Wn,"natural frequency,Wn=")
//2*zeta*Wn=c(1,2)
zeta=c(1,2)/(2*Wn)//damping ratio
disp(zeta,"damping ratio,zeta=")
Wd=Wn*sqrt(1-zeta^2)//damped frequency
disp(Wd,"damping ratio,Wd=")
Tp=%pi/Wd//peak time
disp(Tp,"peak time,Tp=")
Mp=(exp(-(zeta*%pi)/sqrt(1-zeta^2)))*100//max. overshoot
disp(Mp,"max overshoot,Mp=")
t=(2*%pi)/(Wn*sqrt(1-zeta^2))//period of oscillation
disp(t,'time at which first overshoot occurs=')
disp(t,"period of oscillation,t=")
ts=4/(zeta*Wn)//settling time
disp(ts,"settling time,ts=")
N=Wd/(2*%pi)*ts//no. of oscillations completed before reaching steady state
disp(N,"no. of oscillations completed before reaching steady state,N=")
|
263508bb6926e89afef4d7fc408e1be3f3f3d2d6
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/991/CH14/EX14.7/Example14_7.sce
|
2257ea51a4b5f76bb9ed9ea23f1aa0f1e7029e2a
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 575 |
sce
|
Example14_7.sce
|
//Example 14.7. refer fig.14.6
clc
format(6)
RL=((40*2)/42)*10^3 //in ohm
disp(RL," R''L(ohm) = RB || RL =")
Av=(-80*1905)/5000
disp(Av," Av = -hfe*R''L / hie =")
format(9)
x1=(40000)/(1+30.48)
Rif=(x1*5000)/(x1+5000) //in ohm
disp(Rif," Rif(ohm) = hie || (RB / 1-Av) =")
format(6)
Avf=(-30.48*1013.172)/(600+1013.172)
disp(Avf," Avf = Vo/Vs = Av*Rif / RS+Rif =")
Rof=(40000/600)*(5600/80) //in ohm
x2=Rof*10^-3 //in k-ohm
disp(x2," Rof(k-ohm) = (RB / RS) * (RS+hie / hfe) =")
Roff=(4.666*2)/(6.666) //in k-ohm
disp(Roff," R''of(k-ohm) = Rof || RL =")
|
3cbbd7a8a717520a5bba27f4abba0be5726fbaf9
|
3b9a879e67cbab4a5a4a5081e2e9c38b3e27a8cc
|
/Área 1/Revisão P1/MetodoNewtonComErroRelativo.sce
|
cc0cb9be11408ec0d599596fa349e0e0340aea62
|
[
"MIT"
] |
permissive
|
JPedroSilveira/numerical-calculus-with-scilab
|
32e04e9b1234a0a82275f86aa2d6416198fa6c81
|
190bc816dfaa73ec2efe289c34baf21191944a53
|
refs/heads/master
| 2023-05-10T22:39:02.550321 | 2021-05-11T17:17:09 | 2021-05-11T17:17:09 | null | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 324 |
sce
|
MetodoNewtonComErroRelativo.sce
|
function [resultado] = erro_relativo(x, xl)
resultado = abs((x-xl)/x)
endfunction
//Método de Newton para f(x) = x - cos(x)
x = 0.7
xl = x
primeira = %T
while primeira | erro_relativo(x,xl) < 10^(-5)
if primeira then
primeira = %F
end
xl = x
x = x - (x - cos(x))/(1 + sin(x))
end
disp(x)
|
c386ee7bc11f9d1f1fb76b49633cb05bbdc6440e
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/964/CH6/EX6.8/6_8.sce
|
0f44bec043805e156d8dcdcd85a0bc404216cb9f
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 426 |
sce
|
6_8.sce
|
//clc()
del = 0.01;
z = 0.56714329
x1 = 1;
//f(x) = exp(-x) - x
disp(x1,"x1 = ")
for i = 1:4
if i == 1 then
x(i) = 1
else
w = x(i-1);
m = exp(-x(i-1)) - x(i-1);
x(i-1) = x(i-1)*(1+del);
n = exp(-x(i-1)) - x(i-1);
x(i) = w - (x(i-1)- w) * m/(n-m);
em = (z - x(i))*100/z;
disp(x(i),"x = ")
disp("%",em,"error = ")
end
end
|
eec52c30e98e228b35188d52e29e8d42f56f7dc7
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2294/CH1/EX1.17/EX1_17.sce
|
806bf7ff61bca0917e05beb65dd4825c7b17e287
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,006 |
sce
|
EX1_17.sce
|
//Example 1.17<i>
//Determine the power and the rms value of the signal
clc;
t=0:0.001:10;
y=5*cos(50*t+%pi/3);
P=(integrate('5^2*(cos(50*t))^2','t',0,2*%pi))/(2*%pi);
rmsvalue=sqrt(P);
disp(P,'The power of the given signal is:');
disp(rmsvalue,'the rms value is:');
//Example 1.17<ii>
//Determine the power amd rms value of the signal
clc;
t=0:0.001:10;
x1=10*sin(50*t+%pi/4);
x2=16*cos(100*t+%pi/3);
P1=(integrate('10^2*(sin(50*t))^2','t',0,2*%pi))/(2*%pi);
P2=(integrate('16^2*(cos(100*t))^2','t',0,2*%pi))/(2*%pi);
P=P1+P2;
rmsvalue=sqrt(P);
disp(P,'The power of the given signal is:');
disp(rmsvalue,'the rms value is:');
//Example 1.17 <iii>
//Determine the power and rms value of the signal
clc;
t=0:0.001:10;
x1=5*cos(15*t);
x2=5*cos(5*t);
P1=(integrate('5^2*(cos(15*t))^2','t',0,2*%pi))/(2*%pi);
P2=(integrate('5^2*(cos(5*t))^2','t',0,2*%pi))/(2*%pi);
P=P1+P2;
rmsvalue=sqrt(P);
disp(P,'The power of the given signal is:');
disp(rmsvalue,'the rms value is:');
|
ed97745c7768a0b91616bf154ab39c7f9e8d4ed1
|
b5801afaa3964cbd7f9c1c8cf732cdcdb020e7fc
|
/Scilab6-Keras-Toolbox/keras_definitions.sce
|
80503f0345188e2aa5ccbc04ef051e9ae9c4dcda
|
[
"BSD-3-Clause"
] |
permissive
|
TanayKarve/scilab-keras-toolbox
|
e179b283102a580f2192d44c63dbc44a6fbaf03d
|
48045cd955c821a00377f9719f21fe0f91148541
|
refs/heads/master
| 2022-12-03T09:22:16.551928 | 2020-08-23T13:26:21 | 2020-08-23T13:26:21 | 289,681,759 | 1 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,606 |
sce
|
keras_definitions.sce
|
mode(-1);
function[]= ANN_train(layers,epochs,batchsize)
dataset = uigetfile(["*.csv"],"~", "Choose a dataset file", %t);
label = input("Enter label column:","string");
disp('Training...');
unix("python3.8 KerasANN.py "+dataset+" "+label+" "+layers+" "+string(epochs)+" "+string(batchsize))
endfunction
function[output]= ANN_test_sample(test_sample)
model_d= unix_g("pwd")+"/models";
model_file = uigetfile(["neural*.ml"],model_d,"Choose a model file", %t);
output= ANN_test(test_sample,int32(length(test_sample)),model_file)
endfunction
function[output]= image_model(epochs)
image_dir = uigetdir("~","Choose an image directory");
disp("Training...");
output = image_train_tl(image_dir,epochs);
printf("Training accuracy: %0.2f",(output*100));
endfunction
function[output]= image_model_test()
model_d= unix_g("pwd")+"/models";
model_file = uigetfile(["image*.ml"],model_d, "Choose a model file", %t);
image_file = uigetfile(["*.jpeg";"*.jpg";"*.png"],"~", "Choose an image file", %t);
output = image_test_tl(image_file,model_file);
disp('The selected image is of:')
disp(output)
endfunction
function[]=plotTrainingAccuracy()
unix_w("python3.8 GetSessionInfo.py accuracy")
unix_w("xdg-open plots/AccuracyPlot.png");
endfunction
function[]=plotTrainingLoss()
unix_w("python3.8 GetSessionInfo.py loss")
unix("xdg-open plots/LossPlot.png");
endfunction
function[]=plotConfusionMatrix()
unix_w("python3.8 GetSessionInfo.py cmat")
unix_w("xdg-open plots/ConfusionMatrixPlot.png");
endfunction
|
1b3b971604e3ac26e8ffadf8a05409c561cdbb94
|
36c5f94ce0d09d8d1cc8d0f9d79ecccaa78036bd
|
/[Pressure] Longbow Highground.sce
|
ae9e36dbc2857f89333f8ad28bab099836b034c2
|
[] |
no_license
|
Ahmad6543/Scenarios
|
cef76bf19d46e86249a6099c01928e4e33db5f20
|
6a4563d241e61a62020f76796762df5ae8817cc8
|
refs/heads/master
| 2023-03-18T23:30:49.653812 | 2020-09-23T06:26:05 | 2020-09-23T06:26:05 | null | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 109,352 |
sce
|
[Pressure] Longbow Highground.sce
|
Name=[Pressure] Longbow Highground
PlayerCharacters=Counter-Striker
BotCharacters=Counter-Striker Bot PEEKER.bot
IsChallenge=true
Timelimit=60.0
PlayerProfile=Counter-Striker
AddedBots=Counter-Striker Bot PEEKER.bot
PlayerMaxLives=0
BotMaxLives=0
PlayerTeam=1
BotTeams=2
MapName=longbow.map
MapScale=3.0
BlockProjectilePredictors=true
BlockCheats=true
InvinciblePlayer=false
InvincibleBots=false
Timescale=1.0
BlockHealthbars=false
TimeRefilledByKill=0.0
ScoreToWin=1.0
ScorePerDamage=10.0
ScorePerKill=100.0
ScorePerMidairDirect=0.0
ScorePerAnyDirect=0.0
ScorePerTime=0.0
ScoreLossPerDamageTaken=1.0
ScoreLossPerDeath=200.0
ScoreLossPerMidairDirected=0.0
ScoreLossPerAnyDirected=0.0
ScoreMultAccuracy=true
ScoreMultDamageEfficiency=true
ScoreMultKillEfficiency=true
GameTag=Apex Legends
WeaponHeroTag=Longbow 1x no stock, Longbow 4x with stock
DifficultyTag=3
AuthorsTag=dock :)
BlockHitMarkers=false
BlockHitSounds=false
BlockMissSounds=false
BlockFCT=false
Description=Longbow 1v1 highground scenario, accuracy is accounted for and so is dmg + death. Feel free to leave feedback :)
GameVersion=1.0.8.0
ScorePerDistance=0.0
MBSEnable=false
MBSTime1=0.25
MBSTime2=0.5
MBSTime3=0.75
MBSTime1Mult=0.9
MBSTime2Mult=0.8
MBSTime3Mult=0.8
MBSFBInstead=false
MBSRequireEnemyAlive=true
[Aim Profile]
Name=High Skill
MinReactionTime=0.25
MaxReactionTime=0.35
MinSelfMovementCorrectionTime=0.001
MaxSelfMovementCorrectionTime=0.05
FlickFOV=30.0
FlickSpeed=1.5
FlickError=10.0
TrackSpeed=5.0
TrackError=2.0
MaxTurnAngleFromPadCenter=75.0
MinRecenterTime=0.3
MaxRecenterTime=0.5
OptimalAimFOV=30.0
OuterAimPenalty=1.0
MaxError=35.0
ShootFOV=15.0
VerticalAimOffset=0.0
MaxTolerableSpread=5.0
MinTolerableSpread=1.0
TolerableSpreadDist=2000.0
MaxSpreadDistFactor=2.0
[Aim Profile]
Name=cs
MinReactionTime=0.18
MaxReactionTime=0.3
MinSelfMovementCorrectionTime=0.007
MaxSelfMovementCorrectionTime=0.035
FlickFOV=10.0
FlickSpeed=1.0
FlickError=3.0
TrackSpeed=3.5
TrackError=3.5
MaxTurnAngleFromPadCenter=90.0
MinRecenterTime=0.25
MaxRecenterTime=0.4
OptimalAimFOV=35.0
OuterAimPenalty=1.1
MaxError=35.0
ShootFOV=1.0
VerticalAimOffset=-5.0
MaxTolerableSpread=2.0
MinTolerableSpread=0.0
TolerableSpreadDist=2000.0
MaxSpreadDistFactor=2.0
[Aim Profile]
Name=Default
MinReactionTime=0.3
MaxReactionTime=0.4
MinSelfMovementCorrectionTime=0.001
MaxSelfMovementCorrectionTime=0.05
FlickFOV=30.0
FlickSpeed=1.5
FlickError=15.0
TrackSpeed=3.5
TrackError=3.5
MaxTurnAngleFromPadCenter=75.0
MinRecenterTime=0.3
MaxRecenterTime=0.5
OptimalAimFOV=30.0
OuterAimPenalty=1.0
MaxError=40.0
ShootFOV=15.0
VerticalAimOffset=0.0
MaxTolerableSpread=5.0
MinTolerableSpread=1.0
TolerableSpreadDist=2000.0
MaxSpreadDistFactor=2.0
[Bot Profile]
Name=Counter-Striker Bot PEEKER
DodgeProfileNames=MidStrafes
DodgeProfileWeights=1.0
DodgeProfileMaxChangeTime=10.0
DodgeProfileMinChangeTime=0.1
WeaponProfileWeights=1.5;1.5;1.5;1.0;1.0;1.0;1.0;1.0
AimingProfileNames=High Skill;High Skill;cs;cs;cs;Default;Default;Default
WeaponSwitchTime=5.0
UseWeapons=true
CharacterProfile=Counting-Striker
SeeThroughWalls=false
NoDodging=false
NoAiming=false
[Character Profile]
Name=Counter-Striker
MaxHealth=100.0
WeaponProfileNames=Longbow 1x no stock;Longbow 4x with stock;;;;;;
MinRespawnDelay=0.0001
MaxRespawnDelay=0.0001
StepUpHeight=75.0
CrouchHeightModifier=0.75
CrouchAnimationSpeed=1.0
CameraOffset=X=0.000 Y=0.000 Z=0.000
HeadshotOnly=false
DamageKnockbackFactor=1.0
MovementType=Base
MaxSpeed=1100.0
MaxCrouchSpeed=250.0
Acceleration=6000.0
AirAcceleration=16000.0
Friction=7.5
BrakingFrictionFactor=1.25
JumpVelocity=800.0
Gravity=2.5
AirControl=1.0
CanCrouch=true
CanPogoJump=false
CanCrouchInAir=false
CanJumpFromCrouch=true
EnemyBodyColor=X=0.546 Y=0.776 Z=0.546
EnemyHeadColor=X=0.608 Y=0.463 Z=0.314
TeamBodyColor=X=0.000 Y=0.000 Z=0.771
TeamHeadColor=X=0.149 Y=0.542 Z=1.000
BlockSelfDamage=true
InvinciblePlayer=false
InvincibleBots=false
BlockTeamDamage=true
AirJumpCount=0
AirJumpVelocity=800.0
MainBBType=Cylindrical
MainBBHeight=210.0
MainBBRadius=35.0
MainBBHasHead=true
MainBBHeadRadius=25.0
MainBBHeadOffset=0.0
MainBBHide=false
ProjBBType=Cylindrical
ProjBBHeight=250.0
ProjBBRadius=35.0
ProjBBHasHead=true
ProjBBHeadRadius=25.0
ProjBBHeadOffset=0.0
ProjBBHide=true
HasJetpack=false
JetpackActivationDelay=0.5
JetpackFullFuelTime=1000.0
JetpackFuelIncPerSec=100.0
JetpackFuelRegensInAir=true
JetpackThrust=6000.0
JetpackMaxZVelocity=600.0
JetpackAirControlWithThrust=0.25
AbilityProfileNames=;;;
HideWeapon=false
AerialFriction=0.0
StrafeSpeedMult=1.0
BackSpeedMult=1.0
RespawnInvulnTime=0.0
BlockedSpawnRadius=256.0
BlockSpawnFOV=0.0
BlockSpawnDistance=0.0
RespawnAnimationDuration=0.0
AllowBufferedJumps=true
BounceOffWalls=false
LeanAngle=0.0
LeanDisplacement=0.0
AirJumpExtraControl=0.0
ForwardSpeedBias=1.0
HealthRegainedonkill=100.0
HealthRegenPerSec=0.0
HealthRegenDelay=0.0
JumpSpeedPenaltyDuration=0.0
JumpSpeedPenaltyPercent=0.0
ThirdPersonCamera=false
TPSArmLength=300.0
TPSOffset=X=0.000 Y=150.000 Z=150.000
BrakingDeceleration=5000.0
VerticalSpawnOffset=0.0
SpawnXOffset=0.0
SpawnYOffset=0.0
InvertBlockedSpawn=false
[Character Profile]
Name=Counting-Striker
MaxHealth=100.0
WeaponProfileNames=R-99 Projectile - H80;Wingman - Projectile - H80;;;;;;
MinRespawnDelay=0.1
MaxRespawnDelay=10.0
StepUpHeight=75.0
CrouchHeightModifier=0.75
CrouchAnimationSpeed=1.0
CameraOffset=X=0.000 Y=0.000 Z=0.000
HeadshotOnly=false
DamageKnockbackFactor=1.0
MovementType=Base
MaxSpeed=200.0
MaxCrouchSpeed=50.0
Acceleration=6000.0
AirAcceleration=16000.0
Friction=7.5
BrakingFrictionFactor=1.25
JumpVelocity=800.0
Gravity=2.5
AirControl=1.0
CanCrouch=true
CanPogoJump=false
CanCrouchInAir=true
CanJumpFromCrouch=true
EnemyBodyColor=X=0.546 Y=0.776 Z=0.546
EnemyHeadColor=X=0.608 Y=0.463 Z=0.314
TeamBodyColor=X=0.000 Y=0.000 Z=0.771
TeamHeadColor=X=0.149 Y=0.542 Z=1.000
BlockSelfDamage=true
InvinciblePlayer=false
InvincibleBots=false
BlockTeamDamage=true
AirJumpCount=0
AirJumpVelocity=800.0
MainBBType=Cylindrical
MainBBHeight=100.0
MainBBRadius=10.0
MainBBHasHead=true
MainBBHeadRadius=7.0
MainBBHeadOffset=0.0
MainBBHide=false
ProjBBType=Cuboid
ProjBBHeight=100.0
ProjBBRadius=10.0
ProjBBHasHead=true
ProjBBHeadRadius=7.0
ProjBBHeadOffset=0.0
ProjBBHide=true
HasJetpack=false
JetpackActivationDelay=0.5
JetpackFullFuelTime=1000.0
JetpackFuelIncPerSec=100.0
JetpackFuelRegensInAir=true
JetpackThrust=6000.0
JetpackMaxZVelocity=600.0
JetpackAirControlWithThrust=0.25
AbilityProfileNames=Run.abilsprint;Slide.abilsprint;;
HideWeapon=false
AerialFriction=0.0
StrafeSpeedMult=1.0
BackSpeedMult=1.0
RespawnInvulnTime=0.0
BlockedSpawnRadius=0.0
BlockSpawnFOV=0.0
BlockSpawnDistance=0.0
RespawnAnimationDuration=0.5
AllowBufferedJumps=true
BounceOffWalls=false
LeanAngle=0.0
LeanDisplacement=0.0
AirJumpExtraControl=0.0
ForwardSpeedBias=1.0
HealthRegainedonkill=0.0
HealthRegenPerSec=0.0
HealthRegenDelay=0.0
JumpSpeedPenaltyDuration=0.0
JumpSpeedPenaltyPercent=0.0
ThirdPersonCamera=false
TPSArmLength=300.0
TPSOffset=X=0.000 Y=150.000 Z=150.000
BrakingDeceleration=2048.0
VerticalSpawnOffset=0.0
SpawnXOffset=0.0
SpawnYOffset=0.0
InvertBlockedSpawn=false
[Dodge Profile]
Name=MidStrafes
MaxTargetDistance=2500.0
MinTargetDistance=750.0
ToggleLeftRight=true
ToggleForwardBack=true
MinLRTimeChange=0.32
MaxLRTimeChange=0.35
MinFBTimeChange=0.25
MaxFBTimeChange=0.6
DamageReactionChangesDirection=true
DamageReactionChanceToIgnore=0.2
DamageReactionMinimumDelay=0.13
DamageReactionMaximumDelay=0.16
DamageReactionCooldown=1.0
DamageReactionThreshold=0.0
DamageReactionResetTimer=0.2
JumpFrequency=0.0
CrouchInAirFrequency=0.0
CrouchOnGroundFrequency=0.5
TargetStrafeOverride=Oppose
TargetStrafeMinDelay=0.13
TargetStrafeMaxDelay=0.18
MinProfileChangeTime=0.0
MaxProfileChangeTime=0.0
MinCrouchTime=0.1
MaxCrouchTime=0.5
MinJumpTime=0.0
MaxJumpTime=0.0
LeftStrafeTimeMult=0.9
RightStrafeTimeMult=1.0
StrafeSwapMinPause=0.0
StrafeSwapMaxPause=0.0
BlockedMovementPercent=0.5
BlockedMovementReactionMin=0.125
BlockedMovementReactionMax=0.2
[Weapon Profile]
Name=Longbow 1x no stock
Type=Projectile
ShotsPerClick=1
DamagePerShot=55.0
KnockbackFactor=4.0
TimeBetweenShots=0.555
Pierces=false
Category=SemiAuto
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=22720.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=22720.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=0.000 Y=0.000 Z=0.000
MaxTravelTime=5.0
MaxHitscanRange=100000.0
GravityScale=1.0
HeadshotCapable=true
HeadshotMultiplier=1.9
MagazineMax=12
AmmoPerShot=1
ReloadTimeFromEmpty=3.1
ReloadTimeFromPartial=2.3
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=25.0
DelayBeforeShot=0.0
HitscanVisualEffect=Tracer
ProjectileGraphic=Rocket
VisualLifetime=0.1
WallParticleEffect=Gunshot
HitParticleEffect=Flare
BounceOffWorld=false
BounceFactor=0.5
BounceCount=0
HomingProjectileAcceleration=0.0
ProjectileEnemyHitRadius=1.0
CanAimDownSight=true
ADSZoomDelay=0.22
ADSZoomSensFactor=0.82
ADSMoveFactor=0.33
ADSStartDelay=0.0
ShootSoundCooldown=0.08
HitSoundCooldown=0.08
HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=4.0
RecoilNegatable=false
DecalType=1
DecalSize=10.0
DelayAfterShooting=0.0
BeamTracksCrosshair=false
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=300.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=0.0
FlatKnockbackVertical=0.0
HitscanRadius=0.0
HitscanVisualRadius=6.0
TaggingDuration=0.0
TaggingMaxFactor=1.0
TaggingHitFactor=1.0
ProjectileTrail=Sparks
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=false
AimPunchAmount=0.0
AimPunchResetTime=0.2
AimPunchCooldown=0.5
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=false
MinimumDecelVelocity=0.0
PSRManualNegation=false
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=12
CancelReloadOnKill=true
FlatKnockbackHorizontalMin=0.0
FlatKnockbackVerticalMin=0.0
ADSScope=100
ADSFOVOverride=71.0
ADSFOVScale=Apex Legends
ADSAllowUserOverrideFOV=true
IsBurstWeapon=false
ForceFirstPersonInADS=true
ZoomBlockedInAir=false
ADSCameraOffsetX=0.0
ADSCameraOffsetY=0.0
ADSCameraOffsetZ=0.0
QuickSwitchTime=0.6
Explosive=false
Radius=500.0
DamageAtCenter=100.0
DamageAtEdge=100.0
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=false
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=false
SpreadSSA=0.0,0.1,0.0,0.0
SpreadSCA=0.0,0.1,0.0,0.0
SpreadMSA=0.0,0.1,0.0,0.0
SpreadMCA=0.0,0.1,0.0,0.0
SpreadSSH=3.0,3.0,5.0,10.0
SpreadSCH=3.0,3.0,-1.0,8.0
SpreadMSH=3.0,3.0,-1.0,8.0
SpreadMCH=3.0,3.0,-1.0,8.0
MaxRecoilUp=5.0
MinRecoilUp=5.0
MinRecoilHoriz=0.0
MaxRecoilHoriz=0.0
FirstShotRecoilMult=1.0
RecoilAutoReset=true
TimeToRecoilPeak=0.15
TimeToRecoilReset=0.15
AAMode=0
AAPreferClosestPlayer=false
AAAlpha=0.05
AAMaxSpeed=1.0
AADeadZone=0.0
AAFOV=30.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=false
TriggerBotDelay=0.0
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=false
PSRLoopStartIndex=0
PSRViewRecoilTracking=0.45
PSRCapUp=9.0
PSRCapRight=4.0
PSRCapLeft=4.0
PSRTimeToPeak=0.175
PSRResetDegreesPerSec=40.0
UsePerBulletSpread=false
PBS0=0.0,0.0
[Weapon Profile]
Name=Longbow 4x with stock
Type=Projectile
ShotsPerClick=1
DamagePerShot=55.0
KnockbackFactor=4.0
TimeBetweenShots=0.555
Pierces=false
Category=SemiAuto
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=25520.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=25520.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=0.000 Y=0.000 Z=0.000
MaxTravelTime=10.0
MaxHitscanRange=100000.0
GravityScale=1.0
HeadshotCapable=true
HeadshotMultiplier=1.9
MagazineMax=12
AmmoPerShot=1
ReloadTimeFromEmpty=3.1
ReloadTimeFromPartial=2.3
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=25.0
DelayBeforeShot=0.0
HitscanVisualEffect=Tracer
ProjectileGraphic=Rocket
VisualLifetime=0.1
WallParticleEffect=Gunshot
HitParticleEffect=Gunshot
BounceOffWorld=false
BounceFactor=0.5
BounceCount=0
HomingProjectileAcceleration=0.0
ProjectileEnemyHitRadius=0.2
CanAimDownSight=true
ADSZoomDelay=0.22
ADSZoomSensFactor=0.282
ADSMoveFactor=0.33
ADSStartDelay=0.0
ShootSoundCooldown=0.08
HitSoundCooldown=0.08
HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=4.0
RecoilNegatable=false
DecalType=1
DecalSize=15.0
DelayAfterShooting=0.0
BeamTracksCrosshair=false
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=300.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=0.0
FlatKnockbackVertical=0.0
HitscanRadius=0.0
HitscanVisualRadius=6.0
TaggingDuration=0.0
TaggingMaxFactor=1.0
TaggingHitFactor=1.0
ProjectileTrail=Sparks
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=false
AimPunchAmount=0.0
AimPunchResetTime=0.2
AimPunchCooldown=0.5
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=false
MinimumDecelVelocity=0.0
PSRManualNegation=false
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=12
CancelReloadOnKill=true
FlatKnockbackHorizontalMin=0.0
FlatKnockbackVerticalMin=0.0
ADSScope=100
ADSFOVOverride=22.5
ADSFOVScale=Apex Legends
ADSAllowUserOverrideFOV=true
IsBurstWeapon=false
ForceFirstPersonInADS=true
ZoomBlockedInAir=false
ADSCameraOffsetX=0.0
ADSCameraOffsetY=0.0
ADSCameraOffsetZ=0.0
QuickSwitchTime=0.1
Explosive=false
Radius=500.0
DamageAtCenter=100.0
DamageAtEdge=100.0
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=false
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=false
SpreadSSA=0.0,0.1,0.0,0.0
SpreadSCA=0.0,0.1,0.0,0.0
SpreadMSA=0.0,0.1,0.0,0.0
SpreadMCA=0.0,0.1,0.0,0.0
SpreadSSH=3.0,3.0,5.0,10.0
SpreadSCH=3.0,3.0,-1.0,8.0
SpreadMSH=3.0,3.0,-1.0,8.0
SpreadMCH=3.0,3.0,-1.0,8.0
MaxRecoilUp=0.7
MinRecoilUp=0.7
MinRecoilHoriz=0.0
MaxRecoilHoriz=0.0
FirstShotRecoilMult=1.0
RecoilAutoReset=true
TimeToRecoilPeak=0.12
TimeToRecoilReset=0.12
AAMode=0
AAPreferClosestPlayer=false
AAAlpha=0.05
AAMaxSpeed=1.0
AADeadZone=0.0
AAFOV=30.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=false
TriggerBotDelay=0.0
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=false
PSRLoopStartIndex=0
PSRViewRecoilTracking=0.45
PSRCapUp=9.0
PSRCapRight=4.0
PSRCapLeft=4.0
PSRTimeToPeak=0.175
PSRResetDegreesPerSec=40.0
UsePerBulletSpread=false
PBS0=0.0,0.0
[Weapon Profile]
Name=R-99 Projectile - H80
Type=Projectile
ShotsPerClick=1
DamagePerShot=12.0
KnockbackFactor=4.0
TimeBetweenShots=0.0555
Pierces=false
Category=FullyAuto
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=21000.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=21000.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=0.000 Y=0.000 Z=0.000
MaxTravelTime=5.0
MaxHitscanRange=100000.0
GravityScale=1.0
HeadshotCapable=true
HeadshotMultiplier=1.12
MagazineMax=30
AmmoPerShot=1
ReloadTimeFromEmpty=2.25
ReloadTimeFromPartial=1.66
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=12.0
DelayBeforeShot=0.0
HitscanVisualEffect=Tracer
ProjectileGraphic=Ball
VisualLifetime=0.1
WallParticleEffect=Gunshot
HitParticleEffect=Blood
BounceOffWorld=false
BounceFactor=0.5
BounceCount=0
HomingProjectileAcceleration=0.0
ProjectileEnemyHitRadius=0.2
CanAimDownSight=true
ADSZoomDelay=0.15
ADSZoomSensFactor=0.87
ADSMoveFactor=0.9
ADSStartDelay=0.0
ShootSoundCooldown=0.03
HitSoundCooldown=0.03
HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=4.0
RecoilNegatable=false
DecalType=1
DecalSize=10.0
DelayAfterShooting=0.0
BeamTracksCrosshair=false
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=300000.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=0.0
FlatKnockbackVertical=0.0
HitscanRadius=0.0
HitscanVisualRadius=6.0
TaggingDuration=0.2
TaggingMaxFactor=0.75
TaggingHitFactor=0.75
ProjectileTrail=Smoke
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=false
AimPunchAmount=0.0
AimPunchResetTime=0.2
AimPunchCooldown=0.5
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=false
MinimumDecelVelocity=0.0
PSRManualNegation=true
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=30
CancelReloadOnKill=true
FlatKnockbackHorizontalMin=0.0
FlatKnockbackVerticalMin=0.0
ADSScope=No Scope
ADSFOVOverride=77.0
ADSFOVScale=Apex Legends
ADSAllowUserOverrideFOV=true
IsBurstWeapon=false
ForceFirstPersonInADS=true
ZoomBlockedInAir=false
ADSCameraOffsetX=0.0
ADSCameraOffsetY=0.0
ADSCameraOffsetZ=0.0
QuickSwitchTime=0.1
Explosive=false
Radius=500.0
DamageAtCenter=100.0
DamageAtEdge=100.0
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=false
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=false
SpreadSSA=0.0,1.0,-1.0,0.0
SpreadSCA=0.0,1.0,-1.0,0.0
SpreadMSA=0.0,1.0,-1.0,0.0
SpreadMCA=0.0,1.0,-1.0,0.0
SpreadSSH=0.4,1.0,1.0,2.0
SpreadSCH=0.4,1.0,0.8,2.0
SpreadMSH=0.4,0.1,1.0,2.0
SpreadMCH=0.4,0.1,1.0,2.0
MaxRecoilUp=0.0
MinRecoilUp=0.0
MinRecoilHoriz=0.0
MaxRecoilHoriz=0.0
FirstShotRecoilMult=1.0
RecoilAutoReset=false
TimeToRecoilPeak=0.05
TimeToRecoilReset=0.35
AAMode=0
AAPreferClosestPlayer=false
AAAlpha=0.05
AAMaxSpeed=1.0
AADeadZone=0.0
AAFOV=30.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=false
TriggerBotDelay=0.0
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=true
PSRLoopStartIndex=0
PSRViewRecoilTracking=1.0
PSRCapUp=34.0
PSRCapRight=34.0
PSRCapLeft=34.0
PSRTimeToPeak=0.175
PSRResetDegreesPerSec=30.0
PSR0=0.547,0.094
PSR1=0.141,0.0
PSR2=0.609,-0.016
PSR3=0.64,-0.141
PSR4=0.593,0.203
PSR5=0.656,0.234
PSR6=0.578,0.39
PSR7=0.375,0.031
PSR8=0.672,0.141
PSR9=0.547,-0.172
PSR10=0.484,-0.422
PSR11=0.344,-0.047
PSR12=0.718,-0.187
PSR13=0.25,0.203
PSR14=0.141,0.156
PSR15=0.094,0.062
PSR16=-0.094,0.437
PSR17=0.328,-0.328
PSR18=0.031,-0.39
PSR19=0.203,-0.25
PSR20=0.125,-0.359
PSR21=0.141,-0.344
PSR22=-0.078,0.187
PSR23=0.062,0.562
PSR24=-0.141,0.344
PSR25=0.086,0.257
PSR26=0.086,0.257
PSR27=0.086,-0.257
PSR28=0.086,-0.257
UsePerBulletSpread=false
PBS0=0.0,0.0
[Weapon Profile]
Name=Wingman - Projectile - H80
Type=Projectile
ShotsPerClick=1
DamagePerShot=45.0
KnockbackFactor=4.0
TimeBetweenShots=0.384
Pierces=false
Category=SemiAuto
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=18000.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=18000.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=100.000 Y=0.000 Z=0.000
MaxTravelTime=5.0
MaxHitscanRange=100000.0
GravityScale=1.0
HeadshotCapable=true
HeadshotMultiplier=1.68
MagazineMax=10
AmmoPerShot=1
ReloadTimeFromEmpty=1.83
ReloadTimeFromPartial=1.83
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=45.0
DelayBeforeShot=0.0
HitscanVisualEffect=Tracer
ProjectileGraphic=Ball
VisualLifetime=0.1
WallParticleEffect=Gunshot
HitParticleEffect=Blood
BounceOffWorld=false
BounceFactor=0.5
BounceCount=0
HomingProjectileAcceleration=0.0
ProjectileEnemyHitRadius=1.5
CanAimDownSight=true
ADSZoomDelay=0.15
ADSZoomSensFactor=0.87
ADSMoveFactor=1.0
ADSStartDelay=0.0
ShootSoundCooldown=0.08
HitSoundCooldown=0.08
HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=4.0
RecoilNegatable=false
DecalType=1
DecalSize=10.0
DelayAfterShooting=0.0
BeamTracksCrosshair=false
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=300000.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=0.0
FlatKnockbackVertical=0.0
HitscanRadius=0.0
HitscanVisualRadius=6.0
TaggingDuration=0.25
TaggingMaxFactor=0.5
TaggingHitFactor=0.5
ProjectileTrail=Smoke
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=false
AimPunchAmount=0.0
AimPunchResetTime=0.2
AimPunchCooldown=0.5
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=false
MinimumDecelVelocity=0.0
PSRManualNegation=false
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=10
CancelReloadOnKill=true
FlatKnockbackHorizontalMin=0.0
FlatKnockbackVerticalMin=0.0
ADSScope=No Scope
ADSFOVOverride=77.0
ADSFOVScale=Apex Legends
ADSAllowUserOverrideFOV=true
IsBurstWeapon=false
ForceFirstPersonInADS=true
ZoomBlockedInAir=false
ADSCameraOffsetX=0.0
ADSCameraOffsetY=0.0
ADSCameraOffsetZ=0.0
QuickSwitchTime=0.1
Explosive=false
Radius=500.0
DamageAtCenter=100.0
DamageAtEdge=100.0
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=false
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=false
SpreadSSA=0.0,0.1,0.0,0.0
SpreadSCA=0.0,0.1,0.0,0.0
SpreadMSA=0.0,0.1,0.0,0.0
SpreadMCA=0.0,0.1,0.0,0.0
SpreadSSH=0.6,1.0,1.0,3.0
SpreadSCH=0.6,1.0,1.0,2.5
SpreadMSH=0.5,0.1,0.3,3.0
SpreadMCH=0.0,0.1,0.0,0.0
MaxRecoilUp=0.0
MinRecoilUp=0.0
MinRecoilHoriz=0.0
MaxRecoilHoriz=0.0
FirstShotRecoilMult=1.0
RecoilAutoReset=false
TimeToRecoilPeak=0.1
TimeToRecoilReset=0.05
AAMode=0
AAPreferClosestPlayer=false
AAAlpha=0.05
AAMaxSpeed=1.0
AADeadZone=0.0
AAFOV=30.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=false
TriggerBotDelay=0.0
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=true
PSRLoopStartIndex=2
PSRViewRecoilTracking=1.0
PSRCapUp=9.0
PSRCapRight=4.0
PSRCapLeft=4.0
PSRTimeToPeak=0.5
PSRResetDegreesPerSec=30.0
PSR0=1.4,0.3
PSR1=0.61,0.23
PSR2=0.2,-0.094
PSR3=0.115,0.146
PSR4=0.0,0.124
PSR5=-0.2,0.2
PSR6=-0.21,-0.05
PSR7=-0.178,-0.084
PSR8=-0.104,-0.115
UsePerBulletSpread=false
PBS0=0.0,0.0
[Sprint Ability Profile]
Name=Run
MaxCharges=1.0
ChargeTimer=0.001
ChargesRefundedOnKill=0.0
DelayAfterUse=0.1
FullyAuto=false
AbilityDuration=0.0
BlockAttackWhileSprinting=false
AbilityBlockedWhenAttacking=false
SpeedModifier=1.6
45DegreeSprint=true
90DegreeSprint=false
135DegreeSprint=false
180DegreeSprint=false
TapToSprint=true
Block45DegreesWhenSprinting=false
AIUseInCombat=true
AIUseOutOfCombat=false
AIUseOnGround=true
AIUseInAir=true
AIReuseTimer=1.0
AIMinSelfHealth=0.0
AIMaxSelfHealth=100.0
AIMinTargHealth=0.0
AIMaxTargHealth=100.0
AIMinTargDist=0.0
AIMaxTargDist=2000.0
AIMaxTargFOV=15.0
AIDamageReaction=true
AIDamageReactionIgnoreChance=0.0
AIDamageReactionMinDelay=0.125
AIDamageReactionMaxDelay=0.25
AIDamageReactionCooldown=1.0
AIDamageReactionThreshold=0.0
AIDamageReactionResetTimer=0.1
[Sprint Ability Profile]
Name=Slide
MaxCharges=1.0
ChargeTimer=2.0
ChargesRefundedOnKill=0.0
DelayAfterUse=3.0
FullyAuto=true
AbilityDuration=0.4
BlockAttackWhileSprinting=false
AbilityBlockedWhenAttacking=false
SpeedModifier=2.25
45DegreeSprint=true
90DegreeSprint=false
135DegreeSprint=true
180DegreeSprint=true
TapToSprint=true
Block45DegreesWhenSprinting=false
AIUseInCombat=true
AIUseOutOfCombat=false
AIUseOnGround=true
AIUseInAir=true
AIReuseTimer=1.0
AIMinSelfHealth=0.0
AIMaxSelfHealth=100.0
AIMinTargHealth=0.0
AIMaxTargHealth=100.0
AIMinTargDist=0.0
AIMaxTargDist=2000.0
AIMaxTargFOV=15.0
AIDamageReaction=true
AIDamageReactionIgnoreChance=0.0
AIDamageReactionMinDelay=0.125
AIDamageReactionMaxDelay=0.25
AIDamageReactionCooldown=1.0
AIDamageReactionThreshold=0.0
AIDamageReactionResetTimer=0.1
[Map Data]
reflex map version 8
global
entity
type WorldSpawn
brush
vertices
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brush
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faces
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brush
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brush
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brush
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faces
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brush
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brush
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brush
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|
ae2948e975300bd874c31b14c7b3c49d8e1d3cca
|
fd6a414e5722e920e5ebe08c77fe0f70b29e77cf
|
/ComparingSTACF.sce
|
bfcc5bf5927cc1bcfcbff0b9f95a7147d12c1438
|
[] |
no_license
|
JBouis/AudioProcessing
|
e774bdfaf38207643d441f975a96773ae3cbbd24
|
c9f81b8d5ce447b014707b309ef209530219adc0
|
refs/heads/master
| 2021-05-18T02:21:40.839402 | 2020-03-29T15:22:16 | 2020-03-29T15:22:16 | 251,063,576 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,145 |
sce
|
ComparingSTACF.sce
|
// Program to fin short Time Autocorrelation Function
// Using Rectangular and Hamming window
clear,close,clear,
[y,Fs]=wavread('C:\Test_Project\a-team_my_way.wav');
beg= 5200; // Sample at which window is to be applied
N= 500; // Length of window in Sample
x=y(beg:beg+N-1); // Obtainin the required segment
whm= window('hm',N); // Hamming window
Ham_seg=x.*whm; // Multiplying window with the signal
wr=window('re',N);// Rectangular Window
Rect_seg=x.*wr;
t=(beg:beg+N-1)/Fs; // Adjusting the x axis to time
subplot(311)
plot(t,Rect_seg)
xlabel('Time in seconds')
title('Selected segment in the signal')
c1= xcorr(Rect_seg); // Autocorrelation
lag=(1:length(c1))-ceil(length(c1)/2);
// Adjusting x axis to get peak at lag=0
subplot(312)
plot(lag,c1)
title('Short Time Autocorrelation using Rectangular window')
xlabel(' Lag k')
ylabel('STACF')
//////////////////
c2=xcorr(Ham_seg);
lag=(1:length(c1))-ceil(length(c2)/2); // Adjusting x axis
// to get peak at lag=0
subplot(313)
plot(lag,c2)
title('Short Time Autocorrelation using Hamming window')
xlabel('Lag k')
ylabel('STACF')
|
ea9aa713d8d542b6542e21bbe74a195046a3989f
|
a62e0da056102916ac0fe63d8475e3c4114f86b1
|
/set5/s_Electrical_And_Electronics_Engineering_Materials_J._B._Gupta_1730.zip/Electrical_And_Electronics_Engineering_Materials_J._B._Gupta_1730/CH4/EX4.2/Exa4_2.sce
|
107fa9c68984cf510697934866010eccdf0887a0
|
[] |
no_license
|
hohiroki/Scilab_TBC
|
cb11e171e47a6cf15dad6594726c14443b23d512
|
98e421ab71b2e8be0c70d67cca3ecb53eeef1df6
|
refs/heads/master
| 2021-01-18T02:07:29.200029 | 2016-04-29T07:01:39 | 2016-04-29T07:01:39 | null | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 231 |
sce
|
Exa4_2.sce
|
errcatch(-1,"stop");mode(2);//Exa 4.2
;
;
//given data :
delVDS=1.5;//in Volt
delID=120;//in uAmpere
delID=delID*10^-6;//in Ampere
rd=delVDS/delID;//in Ohm
disp(rd*10^-3,"AC drain Resistance of JFET in Kohm : ");
exit();
|
c215f1dc4805a5675469babc43e537a071964021
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/181/CH2/EX2.5/example2_5.sce
|
badaddb891b62123bc47de70610dada271f73da0
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 955 |
sce
|
example2_5.sce
|
// Find depletion layer capacitance
// Basic Electronics
// By Debashis De
// First Edition, 2010
// Dorling Kindersley Pvt. Ltd. India
// Example 2-5 in page 86
clear; clc; close;
// Given data
epsln=12/(36*%pi*10^11); // Constant for Si in F/cm
A=8.11058*10^-1; // Cross sectional area in m^2
mu_p=500; // Mobility of holes
e=1.6*10^-19; // Charge on an electron in C
V_j=4.9; // Junction potential in V
// Calculation
printf("(a)We have C_t/A = sqrt((e*epsnl)/2)*sqrt(Na/Vj)\n");
K=sqrt((e*epsln)/2);
printf("sqrt((e*epsln)/2) = %0.2e\n",K);
printf("Hence C_t = %0.2e * sqrt(Na/Vj) F/cm^2\n",K);
K1=K*10^12;
printf("Or C_t = %0.2e * sqrt(Na/Vj) pF/cm^2\n",K1);
N_A=1/(3*mu_p*e);
C_T=(2.9*10^-4)*sqrt(N_A/V_j)*(8.14*10^-3);
printf("(b)The depletion layer capacitance = %0.2f pF",C_T);
// Result
// (a) The expression for depletion layer capacitance is proved
// (b) The depletion layer capacitance in silicon is 68.84 pF
|
96b600b2f9c760ed47f777d97ba28e7d65b20985
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3685/CH19/EX19.21/Ex19_21.sce
|
b8bd2ee946076e2df50a4c6ffee85fa51846fe40
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 740 |
sce
|
Ex19_21.sce
|
clc
// Given that
m = 2.5 // Mass flow rate in kg/s
p1 = 1 // Inlet pressure in bar
T1 = 300 // Inlet temperature in bar
n_s = 0.88 // Stage efficiency
Wc = 600 // Power input in kW
delta_t = 21 // Temperature rise in first stage in degree centigrade
gama = 1.4 // Ratio of heat capacities
cp = 1.005 // Heat capacity in kJ/kgK
printf("\n Example 19.21\n")
x = n_s*gama/(gama-1)// Where x = (n/(n-1))
T = Wc/(m*cp)+T1
p = p1*((T/T1)^(x))
T2 = T1 + n_s*delta_t
r = ((T2/T1)^(gama/(gama-1)))// Where r = p2/p1
N = log(p/p1)/log(r)
N_ = ceil(N)
Ts = T1*(p/p1)^((gama-1)/gama)
n_inter = (Ts-T1)/(T-T1)
printf("\n The delivery pressure = %f bar,\n The no of stages = %d,\n The internal efficiency = %f ",p,N_,n_inter)
|
b6682f0f270a44129c05df6eabdaf2c9d1f9e4fa
|
1bb72df9a084fe4f8c0ec39f778282eb52750801
|
/test/TEC5.prev.tst
|
5fa7eaecb00d61365ad2b948ab08ee8d1fe39aa4
|
[
"Apache-2.0",
"LicenseRef-scancode-unknown-license-reference"
] |
permissive
|
gfis/ramath
|
498adfc7a6d353d4775b33020fdf992628e3fbff
|
b09b48639ddd4709ffb1c729e33f6a4b9ef676b5
|
refs/heads/master
| 2023-08-17T00:10:37.092379 | 2023-08-04T07:48:00 | 2023-08-04T07:48:00 | 30,116,803 | 2 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 15,401 |
tst
|
TEC5.prev.tst
|
Expanding for base=2, level=7, reasons+features=base,similiar invall,norm
Refined variables=x,y
[0+1x,0+1y]: unknown -> [1] [0,0] x²-y³+2
---------------- level 0
expanding queue[0]^-1,meter=[2,2]: x²-y³+2
[1+2x,1+2y]: unknown -> [1] [1,1] 2x+2x²-3y-6y²-4y³+1
endexp[0]
---------------- level 1
expanding queue[1]^0,meter=[2,2]: 2x+2x²-3y-6y²-4y³+1
[1+4x,3+4y]: unknown -> [2] [0,1] 2x+4x²-27y-36y²-16y³-6
-> solution [5,3],NONTRIVIAL
[3+4x,3+4y]: unknown -> [3] [1,1] 6x+4x²-27y-36y²-16y³-4
endexp[1]
---------------- level 2
expanding queue[2]^1,meter=[2,2]: 2x+4x²-27y-36y²-16y³-6
[1+8x,3+8y]: unknown -> [4] [0,0] 2x+8x²-27y-72y²-64y³-3
[5+8x,3+8y]: unknown -> [5] [1,0] 10x+8x²-27y-72y²-64y³
-> solution [5,3],NONTRIVIAL
endexp[2]
expanding queue[3]^1,meter=[2,2]: 6x+4x²-27y-36y²-16y³-4
[3+8x,3+8y]: unknown -> [6] [0,0] 6x+8x²-27y-72y²-64y³-2
[7+8x,3+8y]: unknown -> [7] [1,0] 14x+8x²-27y-72y²-64y³+3
endexp[3]
---------------- level 3
expanding queue[4]^2,meter=[2,2]: 2x+8x²-27y-72y²-64y³-3
[1+16x,11+16y]: unknown -> [8] [0,1] 2x+16x²-363y-528y²-256y³-83
[9+16x,11+16y]: unknown -> [9] [1,1] 18x+16x²-363y-528y²-256y³-78
endexp[4]
expanding queue[5]^2,meter=[2,2]: 10x+8x²-27y-72y²-64y³
[5+16x,3+16y]: unknown -> [10] [0,0] 10x+16x²-27y-144y²-256y³
-> solution [5,3],NONTRIVIAL
[13+16x,3+16y]: unknown -> [11] [1,0] 26x+16x²-27y-144y²-256y³+9
endexp[5]
expanding queue[6]^3,meter=[2,2]: 6x+8x²-27y-72y²-64y³-2
[3+16x,3+16y]: unknown -> [12] [0,0] 6x+16x²-27y-144y²-256y³-1
[11+16x,3+16y]: unknown -> [13] [1,0] 22x+16x²-27y-144y²-256y³+6
endexp[6]
expanding queue[7]^3,meter=[2,2]: 14x+8x²-27y-72y²-64y³+3
[7+16x,11+16y]: unknown -> [14] [0,1] 14x+16x²-363y-528y²-256y³-80
[15+16x,11+16y]: unknown -> [15] [1,1] 30x+16x²-363y-528y²-256y³-69
endexp[7]
---------------- level 4
expanding queue[8]^4,meter=[2,2]: 2x+16x²-363y-528y²-256y³-83
[1+32x,27+32y]: unknown -> [16] [0,1] 2x+32x²-2187y-2592y²-1024y³-615
[17+32x,27+32y]: unknown -> [17] [1,1] 34x+32x²-2187y-2592y²-1024y³-606
endexp[8]
expanding queue[9]^4,meter=[2,2]: 18x+16x²-363y-528y²-256y³-78
[9+32x,11+32y]: unknown -> [18] [0,0] 18x+32x²-363y-1056y²-1024y³-39
[25+32x,11+32y]: unknown -> [19] [1,0] 50x+32x²-363y-1056y²-1024y³-22
endexp[9]
expanding queue[10]^5,meter=[2,2]: 10x+16x²-27y-144y²-256y³
[5+32x,3+32y]: unknown -> [20] [0,0] 10x+32x²-27y-288y²-1024y³
-> solution [5,3],NONTRIVIAL
[21+32x,3+32y]: unknown -> [21] [1,0] 42x+32x²-27y-288y²-1024y³+13
endexp[10]
expanding queue[11]^5,meter=[2,2]: 26x+16x²-27y-144y²-256y³+9
[13+32x,19+32y]: unknown -> [22] [0,1] 26x+32x²-1083y-1824y²-1024y³-209
[29+32x,19+32y]: unknown -> [23] [1,1] 58x+32x²-1083y-1824y²-1024y³-188
endexp[11]
expanding queue[12]^6,meter=[2,2]: 6x+16x²-27y-144y²-256y³-1
[3+32x,19+32y]: unknown -> [24] [0,1] 6x+32x²-1083y-1824y²-1024y³-214
[19+32x,19+32y]: unknown -> [25] [1,1] 38x+32x²-1083y-1824y²-1024y³-203
endexp[12]
expanding queue[13]^6,meter=[2,2]: 22x+16x²-27y-144y²-256y³+6
[11+32x,3+32y]: unknown -> [26] [0,0] 22x+32x²-27y-288y²-1024y³+3
[27+32x,3+32y]: unknown -> [27] [1,0] 54x+32x²-27y-288y²-1024y³+22
endexp[13]
expanding queue[14]^7,meter=[2,2]: 14x+16x²-363y-528y²-256y³-80
[7+32x,11+32y]: unknown -> [28] [0,0] 14x+32x²-363y-1056y²-1024y³-40
[23+32x,11+32y]: unknown -> [29] [1,0] 46x+32x²-363y-1056y²-1024y³-25
endexp[14]
expanding queue[15]^7,meter=[2,2]: 30x+16x²-363y-528y²-256y³-69
[15+32x,27+32y]: unknown -> [30] [0,1] 30x+32x²-2187y-2592y²-1024y³-608
[31+32x,27+32y]: unknown -> [31] [1,1] 62x+32x²-2187y-2592y²-1024y³-585
endexp[15]
---------------- level 5
expanding queue[16]^8,meter=[2,2]: 2x+32x²-2187y-2592y²-1024y³-615
[1+64x,59+64y]: unknown -> [32] [0,1] 2x+64x²-10443y-11328y²-4096y³-3209
[33+64x,59+64y]: unknown -> [33] [1,1] 66x+64x²-10443y-11328y²-4096y³-3192
endexp[16]
expanding queue[17]^8,meter=[2,2]: 34x+32x²-2187y-2592y²-1024y³-606
[17+64x,27+64y]: unknown -> [34] [0,0] 34x+64x²-2187y-5184y²-4096y³-303
[49+64x,27+64y]: unknown -> [35] [1,0] 98x+64x²-2187y-5184y²-4096y³-270
endexp[17]
expanding queue[18]^9,meter=[2,2]: 18x+32x²-363y-1056y²-1024y³-39
[9+64x,43+64y]: unknown -> [36] [0,1] 18x+64x²-5547y-8256y²-4096y³-1241
[41+64x,43+64y]: unknown -> [37] [1,1] 82x+64x²-5547y-8256y²-4096y³-1216
endexp[18]
expanding queue[19]^9,meter=[2,2]: 50x+32x²-363y-1056y²-1024y³-22
[25+64x,11+64y]: unknown -> [38] [0,0] 50x+64x²-363y-2112y²-4096y³-11
[57+64x,11+64y]: unknown -> [39] [1,0] 114x+64x²-363y-2112y²-4096y³+30
endexp[19]
expanding queue[20]^10,meter=[2,2]: 10x+32x²-27y-288y²-1024y³
[5+64x,3+64y]: unknown -> [40] [0,0] 10x+64x²-27y-576y²-4096y³
-> solution [5,3],NONTRIVIAL
[37+64x,3+64y]: unknown -> [41] [1,0] 74x+64x²-27y-576y²-4096y³+21
endexp[20]
expanding queue[21]^10,meter=[2,2]: 42x+32x²-27y-288y²-1024y³+13
[21+64x,35+64y]: unknown -> [42] [0,1] 42x+64x²-3675y-6720y²-4096y³-663
[53+64x,35+64y]: unknown -> [43] [1,1] 106x+64x²-3675y-6720y²-4096y³-626
endexp[21]
expanding queue[22]^11,meter=[2,2]: 26x+32x²-1083y-1824y²-1024y³-209
[13+64x,51+64y]: unknown -> [44] [0,1] 26x+64x²-7803y-9792y²-4096y³-2070
[45+64x,51+64y]: unknown -> [45] [1,1] 90x+64x²-7803y-9792y²-4096y³-2041
endexp[22]
expanding queue[23]^11,meter=[2,2]: 58x+32x²-1083y-1824y²-1024y³-188
[29+64x,19+64y]: unknown -> [46] [0,0] 58x+64x²-1083y-3648y²-4096y³-94
[61+64x,19+64y]: unknown -> [47] [1,0] 122x+64x²-1083y-3648y²-4096y³-49
endexp[23]
expanding queue[24]^12,meter=[2,2]: 6x+32x²-1083y-1824y²-1024y³-214
[3+64x,19+64y]: unknown -> [48] [0,0] 6x+64x²-1083y-3648y²-4096y³-107
[35+64x,19+64y]: unknown -> [49] [1,0] 70x+64x²-1083y-3648y²-4096y³-88
endexp[24]
expanding queue[25]^12,meter=[2,2]: 38x+32x²-1083y-1824y²-1024y³-203
[19+64x,51+64y]: unknown -> [50] [0,1] 38x+64x²-7803y-9792y²-4096y³-2067
[51+64x,51+64y]: unknown -> [51] [1,1] 102x+64x²-7803y-9792y²-4096y³-2032
endexp[25]
expanding queue[26]^13,meter=[2,2]: 22x+32x²-27y-288y²-1024y³+3
[11+64x,35+64y]: unknown -> [52] [0,1] 22x+64x²-3675y-6720y²-4096y³-668
[43+64x,35+64y]: unknown -> [53] [1,1] 86x+64x²-3675y-6720y²-4096y³-641
endexp[26]
expanding queue[27]^13,meter=[2,2]: 54x+32x²-27y-288y²-1024y³+22
[27+64x,3+64y]: unknown -> [54] [0,0] 54x+64x²-27y-576y²-4096y³+11
[59+64x,3+64y]: unknown -> [55] [1,0] 118x+64x²-27y-576y²-4096y³+54
endexp[27]
expanding queue[28]^14,meter=[2,2]: 14x+32x²-363y-1056y²-1024y³-40
[7+64x,11+64y]: unknown -> [56] [0,0] 14x+64x²-363y-2112y²-4096y³-20
[39+64x,11+64y]: unknown -> [57] [1,0] 78x+64x²-363y-2112y²-4096y³+3
endexp[28]
expanding queue[29]^14,meter=[2,2]: 46x+32x²-363y-1056y²-1024y³-25
[23+64x,43+64y]: unknown -> [58] [0,1] 46x+64x²-5547y-8256y²-4096y³-1234
[55+64x,43+64y]: unknown -> [59] [1,1] 110x+64x²-5547y-8256y²-4096y³-1195
endexp[29]
expanding queue[30]^15,meter=[2,2]: 30x+32x²-2187y-2592y²-1024y³-608
[15+64x,27+64y]: unknown -> [60] [0,0] 30x+64x²-2187y-5184y²-4096y³-304
[47+64x,27+64y]: unknown -> [61] [1,0] 94x+64x²-2187y-5184y²-4096y³-273
endexp[30]
expanding queue[31]^15,meter=[2,2]: 62x+32x²-2187y-2592y²-1024y³-585
[31+64x,59+64y]: unknown -> [62] [0,1] 62x+64x²-10443y-11328y²-4096y³-3194
[63+64x,59+64y]: unknown -> [63] [1,1] 126x+64x²-10443y-11328y²-4096y³-3147
endexp[31]
---------------- level 6
expanding queue[32]^16,meter=[2,2]: 2x+64x²-10443y-11328y²-4096y³-3209
[1+128x,123+128y]: unknown -> [64] [0,1] 2x+128x²-45387y-47232y²-16384y³-14538
[65+128x,123+128y]: unknown -> [65] [1,1] 130x+128x²-45387y-47232y²-16384y³-14505
endexp[32]
expanding queue[33]^16,meter=[2,2]: 66x+64x²-10443y-11328y²-4096y³-3192
[33+128x,59+128y]: unknown -> [66] [0,0] 66x+128x²-10443y-22656y²-16384y³-1596
[97+128x,59+128y]: unknown -> [67] [1,0] 194x+128x²-10443y-22656y²-16384y³-1531
endexp[33]
expanding queue[34]^17,meter=[2,2]: 34x+64x²-2187y-5184y²-4096y³-303
[17+128x,91+128y]: unknown -> [68] [0,1] 34x+128x²-24843y-34944y²-16384y³-5885
[81+128x,91+128y]: unknown -> [69] [1,1] 162x+128x²-24843y-34944y²-16384y³-5836
endexp[34]
expanding queue[35]^17,meter=[2,2]: 98x+64x²-2187y-5184y²-4096y³-270
[49+128x,27+128y]: unknown -> [70] [0,0] 98x+128x²-2187y-10368y²-16384y³-135
[113+128x,27+128y]: unknown -> [71] [1,0] 226x+128x²-2187y-10368y²-16384y³-54
endexp[35]
expanding queue[36]^18,meter=[2,2]: 18x+64x²-5547y-8256y²-4096y³-1241
[9+128x,107+128y]: unknown -> [72] [0,1] 18x+128x²-34347y-41088y²-16384y³-9570
[73+128x,107+128y]: unknown -> [73] [1,1] 146x+128x²-34347y-41088y²-16384y³-9529
endexp[36]
expanding queue[37]^18,meter=[2,2]: 82x+64x²-5547y-8256y²-4096y³-1216
[41+128x,43+128y]: unknown -> [74] [0,0] 82x+128x²-5547y-16512y²-16384y³-608
[105+128x,43+128y]: unknown -> [75] [1,0] 210x+128x²-5547y-16512y²-16384y³-535
endexp[37]
expanding queue[38]^19,meter=[2,2]: 50x+64x²-363y-2112y²-4096y³-11
[25+128x,75+128y]: unknown -> [76] [0,1] 50x+128x²-16875y-28800y²-16384y³-3291
[89+128x,75+128y]: unknown -> [77] [1,1] 178x+128x²-16875y-28800y²-16384y³-3234
endexp[38]
expanding queue[39]^19,meter=[2,2]: 114x+64x²-363y-2112y²-4096y³+30
[57+128x,11+128y]: unknown -> [78] [0,0] 114x+128x²-363y-4224y²-16384y³+15
[121+128x,11+128y]: unknown -> [79] [1,0] 242x+128x²-363y-4224y²-16384y³+104
endexp[39]
expanding queue[40]^20,meter=[2,2]: 10x+64x²-27y-576y²-4096y³
[5+128x,3+128y]: unknown -> [80] [0,0] 10x+128x²-27y-1152y²-16384y³
-> solution [5,3],NONTRIVIAL
[69+128x,3+128y]: unknown -> [81] [1,0] 138x+128x²-27y-1152y²-16384y³+37
endexp[40]
expanding queue[41]^20,meter=[2,2]: 74x+64x²-27y-576y²-4096y³+21
[37+128x,67+128y]: unknown -> [82] [0,1] 74x+128x²-13467y-25728y²-16384y³-2339
[101+128x,67+128y]: unknown -> [83] [1,1] 202x+128x²-13467y-25728y²-16384y³-2270
endexp[41]
expanding queue[42]^21,meter=[2,2]: 42x+64x²-3675y-6720y²-4096y³-663
[21+128x,99+128y]: unknown -> [84] [0,1] 42x+128x²-29403y-38016y²-16384y³-7577
[85+128x,99+128y]: unknown -> [85] [1,1] 170x+128x²-29403y-38016y²-16384y³-7524
endexp[42]
expanding queue[43]^21,meter=[2,2]: 106x+64x²-3675y-6720y²-4096y³-626
[53+128x,35+128y]: unknown -> [86] [0,0] 106x+128x²-3675y-13440y²-16384y³-313
[117+128x,35+128y]: unknown -> [87] [1,0] 234x+128x²-3675y-13440y²-16384y³-228
endexp[43]
expanding queue[44]^22,meter=[2,2]: 26x+64x²-7803y-9792y²-4096y³-2070
[13+128x,51+128y]: unknown -> [88] [0,0] 26x+128x²-7803y-19584y²-16384y³-1035
[77+128x,51+128y]: unknown -> [89] [1,0] 154x+128x²-7803y-19584y²-16384y³-990
endexp[44]
expanding queue[45]^22,meter=[2,2]: 90x+64x²-7803y-9792y²-4096y³-2041
[45+128x,115+128y]: unknown -> [90] [0,1] 90x+128x²-39675y-44160y²-16384y³-11866
[109+128x,115+128y]: unknown -> [91] [1,1] 218x+128x²-39675y-44160y²-16384y³-11789
endexp[45]
expanding queue[46]^23,meter=[2,2]: 58x+64x²-1083y-3648y²-4096y³-94
[29+128x,19+128y]: unknown -> [92] [0,0] 58x+128x²-1083y-7296y²-16384y³-47
[93+128x,19+128y]: unknown -> [93] [1,0] 186x+128x²-1083y-7296y²-16384y³+14
endexp[46]
expanding queue[47]^23,meter=[2,2]: 122x+64x²-1083y-3648y²-4096y³-49
[61+128x,83+128y]: unknown -> [94] [0,1] 122x+128x²-20667y-31872y²-16384y³-4438
[125+128x,83+128y]: unknown -> [95] [1,1] 250x+128x²-20667y-31872y²-16384y³-4345
endexp[47]
expanding queue[48]^24,meter=[2,2]: 6x+64x²-1083y-3648y²-4096y³-107
[3+128x,83+128y]: unknown -> [96] [0,1] 6x+128x²-20667y-31872y²-16384y³-4467
[67+128x,83+128y]: unknown -> [97] [1,1] 134x+128x²-20667y-31872y²-16384y³-4432
endexp[48]
expanding queue[49]^24,meter=[2,2]: 70x+64x²-1083y-3648y²-4096y³-88
[35+128x,19+128y]: unknown -> [98] [0,0] 70x+128x²-1083y-7296y²-16384y³-44
[99+128x,19+128y]: unknown -> [99] [1,0] 198x+128x²-1083y-7296y²-16384y³+23
endexp[49]
expanding queue[50]^25,meter=[2,2]: 38x+64x²-7803y-9792y²-4096y³-2067
[19+128x,115+128y]: unknown -> [100] [0,1] 38x+128x²-39675y-44160y²-16384y³-11879
[83+128x,115+128y]: unknown -> [101] [1,1] 166x+128x²-39675y-44160y²-16384y³-11828
endexp[50]
expanding queue[51]^25,meter=[2,2]: 102x+64x²-7803y-9792y²-4096y³-2032
[51+128x,51+128y]: unknown -> [102] [0,0] 102x+128x²-7803y-19584y²-16384y³-1016
[115+128x,51+128y]: unknown -> [103] [1,0] 230x+128x²-7803y-19584y²-16384y³-933
endexp[51]
expanding queue[52]^26,meter=[2,2]: 22x+64x²-3675y-6720y²-4096y³-668
[11+128x,35+128y]: unknown -> [104] [0,0] 22x+128x²-3675y-13440y²-16384y³-334
[75+128x,35+128y]: unknown -> [105] [1,0] 150x+128x²-3675y-13440y²-16384y³-291
endexp[52]
expanding queue[53]^26,meter=[2,2]: 86x+64x²-3675y-6720y²-4096y³-641
[43+128x,99+128y]: unknown -> [106] [0,1] 86x+128x²-29403y-38016y²-16384y³-7566
[107+128x,99+128y]: unknown -> [107] [1,1] 214x+128x²-29403y-38016y²-16384y³-7491
endexp[53]
expanding queue[54]^27,meter=[2,2]: 54x+64x²-27y-576y²-4096y³+11
[27+128x,67+128y]: unknown -> [108] [0,1] 54x+128x²-13467y-25728y²-16384y³-2344
[91+128x,67+128y]: unknown -> [109] [1,1] 182x+128x²-13467y-25728y²-16384y³-2285
endexp[54]
expanding queue[55]^27,meter=[2,2]: 118x+64x²-27y-576y²-4096y³+54
[59+128x,3+128y]: unknown -> [110] [0,0] 118x+128x²-27y-1152y²-16384y³+27
[123+128x,3+128y]: unknown -> [111] [1,0] 246x+128x²-27y-1152y²-16384y³+118
endexp[55]
expanding queue[56]^28,meter=[2,2]: 14x+64x²-363y-2112y²-4096y³-20
[7+128x,11+128y]: unknown -> [112] [0,0] 14x+128x²-363y-4224y²-16384y³-10
[71+128x,11+128y]: unknown -> [113] [1,0] 142x+128x²-363y-4224y²-16384y³+29
endexp[56]
expanding queue[57]^28,meter=[2,2]: 78x+64x²-363y-2112y²-4096y³+3
[39+128x,75+128y]: unknown -> [114] [0,1] 78x+128x²-16875y-28800y²-16384y³-3284
[103+128x,75+128y]: unknown -> [115] [1,1] 206x+128x²-16875y-28800y²-16384y³-3213
endexp[57]
expanding queue[58]^29,meter=[2,2]: 46x+64x²-5547y-8256y²-4096y³-1234
[23+128x,43+128y]: unknown -> [116] [0,0] 46x+128x²-5547y-16512y²-16384y³-617
[87+128x,43+128y]: unknown -> [117] [1,0] 174x+128x²-5547y-16512y²-16384y³-562
endexp[58]
expanding queue[59]^29,meter=[2,2]: 110x+64x²-5547y-8256y²-4096y³-1195
[55+128x,107+128y]: unknown -> [118] [0,1] 110x+128x²-34347y-41088y²-16384y³-9547
[119+128x,107+128y]: unknown -> [119] [1,1] 238x+128x²-34347y-41088y²-16384y³-9460
endexp[59]
expanding queue[60]^30,meter=[2,2]: 30x+64x²-2187y-5184y²-4096y³-304
[15+128x,27+128y]: unknown -> [120] [0,0] 30x+128x²-2187y-10368y²-16384y³-152
[79+128x,27+128y]: unknown -> [121] [1,0] 158x+128x²-2187y-10368y²-16384y³-105
endexp[60]
expanding queue[61]^30,meter=[2,2]: 94x+64x²-2187y-5184y²-4096y³-273
[47+128x,91+128y]: unknown -> [122] [0,1] 94x+128x²-24843y-34944y²-16384y³-5870
[111+128x,91+128y]: unknown -> [123] [1,1] 222x+128x²-24843y-34944y²-16384y³-5791
endexp[61]
expanding queue[62]^31,meter=[2,2]: 62x+64x²-10443y-11328y²-4096y³-3194
[31+128x,59+128y]: unknown -> [124] [0,0] 62x+128x²-10443y-22656y²-16384y³-1597
[95+128x,59+128y]: unknown -> [125] [1,0] 190x+128x²-10443y-22656y²-16384y³-1534
endexp[62]
expanding queue[63]^31,meter=[2,2]: 126x+64x²-10443y-11328y²-4096y³-3147
[63+128x,123+128y]: unknown -> [126] [0,1] 126x+128x²-45387y-47232y²-16384y³-14507
[127+128x,123+128y]: unknown -> [127] [1,1] 254x+128x²-45387y-47232y²-16384y³-14412
endexp[63]
---------------- level 7
Maximum level 7 [128] mod 2: x²-y³+2
|
e47bcb4d71176617286fd433cce069fd2112442c
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/689/CH11/EX11.3/3.sce
|
fef0b6a7e66389dc74ce0cbde342566f526ada2a
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 526 |
sce
|
3.sce
|
clc; funcprot(0);
//Example 11.3 Lift at subsonic speed
// Initialisation of variables
alp_z = -4; //Angle of attack at zero lift
M16 = 0.16;
Cl = 0.3;
alp = 1.5;
M0 = 0;
M65 = 0.65;
alp25 = 2.5;
// Calculations
//At M = 1.6
DCl_by_Dalp16 = Cl/(alp-alp_z);
//At M = 0
DCl_by_Dalp0 = DCl_by_Dalp16*sqrt(1-M16^2);
////At M = 0.65
DCl_by_Dalp65 = DCl_by_Dalp0/sqrt(1-M65^2);
Cl25 = (alp25 - alp_z)*DCl_by_Dalp65;
//Results
disp(Cl25,"Lift Coefficient at alpha = 2.5 degree: ") ;
|
17647f053d4efafeafca59d35ec3669333415fb3
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3542/CH8/EX8.1/Ex8_1.sce
|
a5348329a337a2a9c70e603d122545d2983e0d91
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 2,224 |
sce
|
Ex8_1.sce
|
// Example no 8.1
// To compute the mean square error distortion and output signal-to-distortion ratio.
// Page no. 420
clc;
clear all;
//Given data
l1=1; // 1st Quantization level
l2=3; // 2nd Quantization level
l3=5; // 3rd Quantization level
l4=7; // 4th Quantization level
U1=(l1+l2)/2; // upper boundary of 1st level
U2=(l2+l3)/2; // upper boundary of 2nd level
U3=(l3+l4)/2; // upper boundary of 3rd level
U4=l4+(U1-l1); // upper boundary of 4th level
L1=l1-(U1-l1); // Lower boundary of 1st level
D1=integrate('(x^3-2*x^2+x)/32','x',L1,U1); // Mean square error distortion of 1st level
D2=integrate('(x^3-6*x^2+9*x)/32','x',U1,U2); // Mean square error distortion of 2nd level
D3=integrate('(x^3-10*x^2+25*x)/32','x',U2,U3); // Mean square error distortion of 3rd level
D4=integrate('(x^3-14*x^2+49*x)/32','x',U3,U4); // Mean square error distortion of 4th level
D=D1+D2+D3+D4; // Total square error distortion
P=integrate('x^3/32','x',L1,U4); // Signal power
SDR=10*log10(P/D); // Output signal-to-distortion ratio.
// Displaying the result in command window
printf('\n The mean square error distortion = %0.3f',D);
printf('\n The output signal-to-distortion ratio = %0.2f dB',SDR);
printf('\n To minimize the distortion, we need to place the quantization levels closer at amplitudes close to 8 and farther at amplitudes close to zero.');
printf('\n This quantizer would be optimal for an input with a uniform pdf.');
|
75d4b2337fef9dd457f4c233d3dd65d4b85b1688
|
5c0124a56cb43a2890e25fbc6e2556d25ff9c4bb
|
/Exercise_17.sce
|
b7103de1269bacfa0dce941a4b7b54203f65dae9
|
[] |
no_license
|
wiiwins/Risk-Management
|
d970aaa2c44409f9c73fd44b8bcfbb25e3e83c3e
|
46c547e9d14019dde274f232fc6354641de245ff
|
refs/heads/master
| 2020-09-01T17:12:36.665964 | 2019-11-26T21:00:32 | 2019-11-26T21:00:32 | 219,013,277 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,576 |
sce
|
Exercise_17.sce
|
// C-Exercise 17
// Jurian Kahl
// Nattawut Phanrattinon
// download distfun package
atomsInstall("distfun");
// Part a)
// Hill estimator function
function alpha = Hill_Estimator(x, k)
y = gsort(x);
alpha = k/sum( log(y(1:(k-1))) - log(y(k)));
endfunction
// Part b)
// Hill plot function
function Hill_Plot(x)
y = x(x>0);
n = length(y);
for k = 2:n
a(k-1) = Hill_Estimator(y, k);
end
plot(2:n, a');
endfunction
// part(c)
scf(0); clf();
m = 3;
N = 500;
lambda = 1;
subplot(3,1,1);
title ("t-distribution with df = 3");
xlabel("k"); ylabel("Hill estimator");
for k=1:m
Hill_Plot(distfun_trnd(3, N, 1));
end
subplot(3,1,2);
title ("t-distribution with df = 8");
xlabel("k"); ylabel("Hill estimator");
for k=1:m
Hill_Plot(distfun_trnd(8, N, 1));
end
subplot(3,1,3);
title ("Exponential distribution with lambda = 1");
xlabel("k"); ylabel("Hill estimator");
for k=1:m
Hill_Plot(grand(N,1,'exp',lambda));
end
// Part d)
// VaR and ES
function [VaR,ES]=VaR_ES_Hill(x,p,k)
N = length(x);
alpha = Hill_Estimator (x,k);
y=gsort(x);
// From section 3.2.3 Equation (3.5)
VaR=(N/k*(1-p))^(-1/alpha)*y(k);
// From section 3.2.4
ES=(1-1/alpha)^(-1)*VaR;
endfunction
// Part e)
data = csvRead('risk1920_Exercise_17_data.dat')
scf(1); clf();
Hill_Plot(data);
title("Hill plot");
//choose k = 40 for reasonable choice since it seems to be constant after some initial oscilations from Hill plot above
p = 0.98;
k = 40;
[VaR,ES]=VaR_ES_Hill(data,p,k)
disp ("for k=40 VaR="+string(VaR)+" ES="+string(ES));
|
2fe1193d8f27a7dcc46875cc67dcc35334f30d29
|
61129043aed87983b640a33b1c260316043fa570
|
/logger/configure.sci
|
dc14a7e643186bc4f08e91d12582046fe76fb9d1
|
[] |
no_license
|
dgerod/gfx4scilab
|
7643dbb42fcbea772af12017dccf484544da6f79
|
4aafc59f241a9383de65e4fb25eefef80660bf64
|
refs/heads/master
| 2021-01-19T03:35:08.368764 | 2017-04-08T06:05:33 | 2017-04-08T06:05:33 | 61,438,380 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 732 |
sci
|
configure.sci
|
// =============================================================================
// gfx4scilab - drawing
// dgerod@xyz-lab.org.es
// =============================================================================
function lg_enable(isOn)
global logCfg;
if isOn == %t then
logCfg.enabled = %t;
else
logCfg.enabled = %f;
end
endfunction
// -----------------------------------------------------------------------------
function lg_setFileMode(isFileMode)
global logCfg;
if isFileMode == %t then
logCfg.logFile.fileType = %t;
else
logCfg.logFile.fileType = %f;
end
endfunction
// =============================================================================
|
b6edd56e6cc2e4af1e52fbf7ea1e9547364c8545
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/980/CH9/EX9.2/9_2.sce
|
b2eea8c17c80d4cb49ff81bab249c5837a8b9f67
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 302 |
sce
|
9_2.sce
|
clc;
clear;
format('e',11);
v=4*10^4;
e=-1.6*10^-19;
Me=9.1*10^-31; //Me=mass of electron.
B=0.4*10^-4;
Wc=-e*B/Me; //Wc=angular frequency.
f=Wc/(2*3.14);
R=v/Wc;
disp(f,"The frequency of the electron(in Hz)=");
disp(R,"The redius of the circle,R(in meter)=");
|
db6a7b137f5c9d59ba4654eccd6468719d806613
|
a62e0da056102916ac0fe63d8475e3c4114f86b1
|
/set8/s_Engineering_Economics_H._Agarwal_1208.zip/Engineering_Economics_H._Agarwal_1208/CH2/EX2.1/Exa1.sce
|
1a6828a777e769b4eef53d58b0a40303951dfbf6
|
[] |
no_license
|
hohiroki/Scilab_TBC
|
cb11e171e47a6cf15dad6594726c14443b23d512
|
98e421ab71b2e8be0c70d67cca3ecb53eeef1df6
|
refs/heads/master
| 2021-01-18T02:07:29.200029 | 2016-04-29T07:01:39 | 2016-04-29T07:01:39 | null | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 240 |
sce
|
Exa1.sce
|
errcatch(-1,"stop");mode(2);//Exa1
;
;
//given data is :
P=10000;//in rupees
n=3;//in years
r=10;//% per annum
A=P*(1+r/100)^n;
CI=A-P;//in rupees
disp("Compound interest is : "+string(CI)+" Rupees.")
exit();
|
7df483b5798e8194e7087b2414b1d98843b8e5a6
|
676ffceabdfe022b6381807def2ea401302430ac
|
/solvers/PulseWaveSolver/Tests/55_Artery_Network.tst
|
90130c6e1ced2d43f458753d3f3634d615f376ae
|
[
"MIT"
] |
permissive
|
mathLab/ITHACA-SEM
|
3adf7a49567040398d758f4ee258276fee80065e
|
065a269e3f18f2fc9d9f4abd9d47abba14d0933b
|
refs/heads/master
| 2022-07-06T23:42:51.869689 | 2022-06-21T13:27:18 | 2022-06-21T13:27:18 | 136,485,665 | 10 | 5 |
MIT
| 2019-05-15T08:31:40 | 2018-06-07T14:01:54 |
Makefile
|
UTF-8
|
Scilab
| false | false | 700 |
tst
|
55_Artery_Network.tst
|
<?xml version="1.0" encoding="utf-8"?>
<test>
<description>55 Artery Network, P=5</description>
<executable>PulseWaveSolver</executable>
<parameters>55_Artery_Network.xml</parameters>
<files>
<file description="Session File">55_Artery_Network.xml</file>
</files>
<metrics>
<metric type="L2" id="1">
<value variable="A" tolerance="1e-12">35.2833</value>
<value variable="u" tolerance="1e-12">66.3241</value>
</metric>
<metric type="Linf" id="2">
<value variable="A" tolerance="1e-12">6.35242</value>
<value variable="u" tolerance="1e-12">22.2798</value>
</metric>
</metrics>
</test>
|
8f803344e83c0c9403cbeb6f3a12c2b3287cd939
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/992/CH2/EX2.7/ex2_7.sce
|
fd2edccef38674c38c3fa2a73303d08282881498
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 276 |
sce
|
ex2_7.sce
|
//Exa:2.7
clc;
clear;
close;
//Given:
m1=0.55;//modulation percent 1
m2=0.65;//modulation percent 2
Pc=360;// in watts
mt=sqrt(m1*m1+m2*m2);
printf("\n\n\t total modulation = %f ",mt);
Pb=(mt*mt)*Pc/2;
printf("\n\n\t total sideband power radiated = %f W",Pb);
|
0445560bac51fffa96c5d6547eae9c90e53457a9
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1271/CH12/EX12.27/example12_27.sce
|
b609a447aedeca61fd394d6eb1a1e6b4190c35eb
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 375 |
sce
|
example12_27.sce
|
clc
// Given that
m1 = 4.00260 // mass of He(4) in a.m.u.
m2 = 0.00055 // mass of electron in a.m.u.
m3 = 12 // mass of C(12) in a.m.u.
// Sample Problem 27 on page no. 12.40
printf("\n # PROBLEM 27 # \n")
printf(" Standard formula used \n")
printf(" del_E = del_m * c^2 \n")
delta_m = 3 * m1 - m3
E = delta_m * 931
printf("\n Energy produce by each reaction is %f MeV.",E)
|
3a074bda2551099e9b7043205de4246a014165ee
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1640/CH5/EX5.8/5_8.sce
|
8fdf9eb10bcff7c305999b2084c67ee0983a861c
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 152 |
sce
|
5_8.sce
|
clc
//initialisation of variables
logh= 0.1761
logk= -0.415
logv= 0.3010
//CALCULATIONS
n= (logh-logk)/logv
//RESULTS
printf ('n = %.2f ',n)
|
ed2fc924c3ed160e2857bc7a4d6678b55d767b2e
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/278/CH10/EX10.15/ex_10_15.sce
|
79776e7fcc0afbef8ed6b47f52663e712ad26822
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 727 |
sce
|
ex_10_15.sce
|
clc
//solution
//given
//ref fig 10.32 and 33
s=6//mm
P=20*10^3//N
l=40//mm
b=90//mm
//let t throat thickness
//let x is distance of Cg from left edge
x=l^2/(2*l+b)//mm
//J=t*[(b+2*l)^3/12-(l^2*(b+l)^2/(b*2*l))]
J=0.707*s*[{(b+2*l)^3/12}-{(l^2*(b+l)^2)/(b+2*l)}]//mm^4
printf("the value of J is,%f mm^4\n",J)
Bg=40
e=200-x//mm
r1=Bg-x//mm
Ab=(90/2)//mm
r2=sqrt(Ab^2+Bg^2)//mm
//cos(q)=r2/r1=0.5625
a=0.5625
A=2*0.707*s*l+(0.707*s*b)//mm^2
t1=P/A//N/mm^2'
t2=P*e*r2/J//N/mm^2
T=sqrt(t1^2 + t2^2 + 2*t1*t2*a)//N/mm^2'
printf( "the value of x is,%f mm\n",x)
printf("the value of direct shear stress is,%f N/mm^2\n",t1)
printf("the value of secondary shear stress is,%f N/mm^2\n",t2)
printf("the max shera stress is,%f N/mm^2",T)
|
8715eb8167a248b6b2fc433d73b33eb0709e9839
|
05db16b4f57b0182fa452e2c11554c3de6fff271
|
/branches/vac4.52_sac_cuda/dev/vac4.52mkg_24_06_2010/scilab/sci_studyfile.sci
|
62839dff635f4a1736caf1360445452434ccb10c
|
[] |
no_license
|
SpungMan/smaug-all
|
09b4fcf6fcec2fc7be1fa85c5c7f2d68c79e504b
|
01df12e98c734529ff984662badc26eaa3a9138b
|
refs/heads/master
| 2021-11-29T14:09:47.094457 | 2018-06-08T09:48:05 | 2018-06-08T09:48:05 | null | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 571 |
sci
|
sci_studyfile.sci
|
function [tree] = sci_studyfile(tree)
// Copyright INRIA (Generated by M2SCI)
// Conversion function for Matlab studyfile()
// Input: tree = Matlab funcall tree
// Ouput: tree = Scilab equivalent for tree
// dims(i,:) is the ith output argument dimensions vector
dims=list(list(1,-1),list(1,-1),list(1,-1),list(1,1))
// dims(i,:) is the ith output argument dimensions vector
vtype=[1;1;1;1]
// prop(i) is the ith output argument property
prop=[0;0;0;0]
for k=1:lhs
tree.lhs(k).dims=dims(k)
tree.lhs(k).vtype=vtype(k)
tree.lhs(k).property=prop(k)
end
endfunction
|
36990e4107f4c4cc7b4bac2cc4480f73d7f34d82
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1904/CH6/EX6.5/6_5.sce
|
221b34fef2a0f8eb9f1560a18d80d982782f730b
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,190 |
sce
|
6_5.sce
|
//To find the pu voltages and tolerable and favourable voltages
//Page 310
clc;
clear;
N=19; //Number Transformers
St=500; //Load on each transformer in kVA
L=5096+(%i*3158); //Load
Vlf=114; //Favourable Voltage
Vlt=111; //Tolerable Volatage
Vb=125; //Base Voltage
//Per Unit Tolerable and favourable voltages
puVlf=Vlf/Vb;
puVlt=Vlt/Vb;
ZM=0.181+(%i*0.115); //The Positive Sequence Impedance
ZTi=0.0086+(%i*0.0492); //Transformer Impedance for 500kVA
ZT=2*ZTi; //Transformer Impedance for 1000kVA
AAF=N*St/abs(L); //Actual Application Factor
printf('\na) The Lowest favourable Voltage is %g pu and The Lowest tolerable voltage is %g pu\n',puVlf,puVlt)
printf('b) There Are No buses in Table 6-5, for the first contingency outage which satisfy the necessary condition\n')
printf('c) For Second Contingency Outage\n')
printf('1) Less than Favourable Voltage are B,C,J,K,R and S\n')
printf('2) Less than Tolerable Voltage are B,C,J,K.\n')
printf('d) ZM/ZT = %g and (1/2)*ZM/ZT = %g respectively.\n',(abs(ZM)/abs(ZT)),(1/2)*(abs(ZM)/abs(ZT)))
printf('The Actual Application Factor is %g\n',AAF)
printf('Therefore the Design of this network is sufficient\n')
|
3cb28c0c49a14a132baef7ce2ab43d568468b3bd
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1133/CH4/EX4.14/Example4_14.sce
|
e7cf930e7fd2cc17484402df6502eec27e7c5de4
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 330 |
sce
|
Example4_14.sce
|
//Example 4.14.
clc
disp("R = 6 k-ohm, C = 1500 pF, R_C = 18 k-ohm")
k=18/6
disp(k,"Now K = R_C / R =")
disp("Therefore, f = 1 / 2*pi*R*C*sqrt(6+4K)")
f=(1/(2*%pi*(6*10^3)*(1500*10^-12)*sqrt(6+12)))*10^-3 // in kHZ
format(6)
disp(f," f(in kHz) =")
hfe=(4*3)+23+(29/3)
disp(hfe," (h_fe)min = 4K + 23 + 29/K =")
|
fdb402a2b41884fca35a11c942703b4f2abd308a
|
009e6209a86f0838f0faca8a33b2c162e5d1a7a6
|
/src/scripts/interpolacionLagrange.sce
|
c5cc2d5f51914f1a7e1822ee0ebf1df973b962c1
|
[] |
no_license
|
MoisesU/MESO-MetodosNumericos
|
90a62a31e3213c50dec55228ceca7ce034cfbb7c
|
17fe0efa1690ac93f36799a12a9f9c99f1ab94a4
|
refs/heads/main
| 2023-06-02T05:51:03.641326 | 2021-06-20T03:18:17 | 2021-06-20T03:18:17 | 306,203,044 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 912 |
sce
|
interpolacionLagrange.sce
|
//Rodríguez Montiel Moisés Ulises
//2NM51
function y = interpolLagrange(funcTab, grado, x)
y = 0
[n, m] = size(funcTab)
if(n <> 2)
error("No es una función tabular")
end
if ~(isreal(funcTab))
error('Elementos no numericos o complejos en el arreglo.');
end
grado = round(grado);
if (or([~isreal(grado), grado <= 0]))
error('El grado tiene que ser un valor entero positivo (mayor a 0).');
end
if grado > m
error('El grado del polinomio es mayor al permitido por el metodo.');
end
for i=1:1:grado
numerador = 1;
denominador = 1;
for j=1:1:grado
if j ~= i
numerador = numerador * (x - funcTab(1, j));
denominador = denominador * (funcTab(1, i) - funcTab(1, j));
end
end
y = y + (numerador/denominador) * funcTab(2, i);
end
endfunction
|
96ef7011c21b2451f7aae90539bfa087322481d6
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2195/CH2/EX2.7.3.a/ex_2_7_3_a.sce
|
f34fa64c6844a089a7a5da09514ba8ed9af5b210
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 327 |
sce
|
ex_2_7_3_a.sce
|
//Example 2.7.3.a: Arithmetic mean
clc;
clear;
close;
//given data :
X1=147.2;// in nF
X2=147.4;// in nF
X3=147.9;// in nF
X4=148.1;// in nF
X5=148.1;// in nF
X6=147.5;// in nF
X7=147.6;// in nF
X8=147.4;// in nF
X9=147.6;// in nF
X10=147.5;// in nF
AM=(X1+X2+X3+X4+X5+X6+X7+X8+X9+X10)/10;
disp(AM,"Arithmetic mean,AM(nF) = ")
|
07c71717d43644c4d14eeb135ce3a666921b70af
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2582/CH5/EX5.12/Ex5_12.sce
|
f8f2e063b4a0213ed71283380157e4994b3d8534
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 438 |
sce
|
Ex5_12.sce
|
//Ex 5.12
clc;clear;close;
format('v',4);
tau=1;//ms
//R1/R2=1.8:9;given range
//Let R1/R2=1.8
R1BYR2=1.8;//ratio
Beta1=1/(R1BYR2+1);
R1BYR2=9;//ratio
Beta2=1/(R1BYR2+1);//unitless
Beta=Beta1:Beta2;//Range of Beta
//For fmin
Tmax=2*log((1+Beta1)/(1-Beta1));//ms
fmin=1000/Tmax;//Hz
//For fmax
Tmin=2*log((1+Beta2)/(1-Beta2));//ms
fmax=1/Tmin;//kHz
disp("Frequency range is "+string(fmin)+" Hz to "+string(fmax)+" kHz");
|
0106f0ca263f86c79046f11f0b304310b58fd613
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3574/CH3/EX3.4/EX3_4.sce
|
1fee5f2253ecd0f41dca0cfdeef678bef85ce971
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 2,176 |
sce
|
EX3_4.sce
|
// Example 3.4
// Determine (a) Circulating current in the paralleled secondaries
// (b) Circulating current as a percent of the rated current of transformer A
// (c) Percent difference in secondary voltage that caused the circulating current
// Page No. 104
clc;
clear;
close;
// Given data
S=100000; // Transformer A and B rating
VLSA=460; // Voltage at the low side of transformer A
VLSB=450; // Voltage at the low side of transformer A
RPUA=0.0136; // Percent resistance of transformer A
XPUA=0.0350; // Percent reactance of transformer A
RPUB=0.0140; // Percent resistance of transformer B
XPUB=0.0332; // Percent reactance of transformer B
// (a) Circulating current in the paralleled secondaries
IA= S/VLSA; // Rated low side current for transformer A
IB= S/VLSB; // Rated low side current for transformer B
ReqA=RPUA*VLSA/IA; // Equivalent resistance of transfomer A
ReqB=RPUB*VLSB/IB; // Equivalent resistance of transfomer B
XeqA=XPUA*VLSA/IA; // Equivalent reactance of transfomer A
XeqB=XPUB*VLSB/IB; // Equivalent reactance of transfomer B
// Impedance of the closed loop formed by two secondaries is
Zloop=ReqA+%i*XeqA+ReqB+%i*XeqB;
// Complex to Polar form...
Zloop_Mag=sqrt(real(Zloop)^2+imag(Zloop)^2); // Magnitude part
Zloop_Ang=atan(imag(Zloop),real(Zloop))*180/%pi; // Angle part
Icirc_Mag=(VLSA-VLSB)/Zloop_Mag; // Circulating current magnitude
Icirc_Ang=0- Zloop_Ang; // Circulating current angle
// (b) Circulating current as a percent of the rated current of transformer A
IcircA=Icirc_Mag*100/IA;
// (c) Percent difference in secondary voltage that caused the circulating current
PD=(VLSA-VLSB)*100/VLSB;
// Display result on command window
printf("\n Circulating current magnitude = %0.1f A ",Icirc_Mag);
printf("\n Circulating current angle = %0.1f deg ",Icirc_Ang);
printf("\n Circulating current as a percent of the rated current = %0.1f Percent ",IcircA);
printf("\n Percent difference in secondary voltage = %0.1f Percent ",PD);
|
6dfcfed440aa82d928ffccf9dabbb4bb96b48e2d
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3012/CH12/EX12.4/Ex12_4.sce
|
31a3b04c6b69257628e1c09314ef3031b6353e14
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 2,255 |
sce
|
Ex12_4.sce
|
// Given:-
y1 = 0.8 // mole fraction of CO2
y2 = 0.2 // mole fraction of O2
T1 = 700.0 // in kelvin
p1 = 5.0 // in bars
V1 = 3.0 // in m/s
p2 = 1.0 // in bars
// Part(a)
// From table A-23
sO2barT1 = 231.358
sCO2barT1 = 250.663
// Calculations
RHS = y2*sO2barT1 + y1*sCO2barT1 + 8.314*log(p2/p1)
// Using table A-23
LHSat510K = y2*221.206 + y1*235.7
LHSat520K = y2*221.812 + y1*236.575
// Using linear interpolation,
T2 = 510 +((520-510)/(LHSat520K-LHSat510K))*(RHS-LHSat510K)
// Result
printf( 'The temperature at the nozzle exit in K is: %f',T2);
// Part(b)
// From table A-23
sbarO2T2 = 221.667 // in kj/kmol.K
sbarO2T1 = 231.358 // in kj/kmol.K
sbarCO2T2 = 236.365 // in kj/kmol.K
sbarCO2T1 = 250.663 // in kj/kmol.K
// Calculations
deltasbarO2 = sbarO2T2-sbarO2T1-8.314*log(p2/p1) // in kj/kmol.K
deltasbarCO2 = sbarCO2T2-sbarCO2T1-8.314*log(p2/p1) // in kj/kmol.K
// Results
printf( 'The entropy changes of the CO2 from inlet to exit, in KJ/Kmol.K is: %f',deltasbarCO2)
printf( 'The entropy change of the O2 from inlet to the exit in kj/kmol.k is: %f',deltasbarO2)
// Part(c)
// From table A-23, the molar specific enthalpies of O2 and CO2 are
h1barO2 = 21184.0
h2barO2 = 15320.0
h1barCO2 = 27125.0
h2barCO2 = 18468.0
// Calculations
M = y1*44.0 + y2*32.0 // apparent molecular weight of the mixture in kg/kmol
deltah = (1.0/M)*(y2*(h1barO2-h2barO2) + y1*(h1barCO2-h2barCO2))
V2 = sqrt(V1**2+ 2*deltah*10**3)
// Result
printf( 'The exit velocity in m/s is: %f',V2)
|
1dc6a42f82b40beb637bebcdac8b3fda293801f8
|
300d1796ae548c978afd104ee7047662b7c75583
|
/Test2.tst
|
d927fd404c5f28c3ab834e1f3d0e7c9b1da0d471
|
[] |
no_license
|
madhavsrms/microservicesedu
|
3b95bd63aadbcb6a5ad97cda26d9def6b36ff46e
|
bb8d6ee272fcf2c2d593748ef7eb385155063500
|
refs/heads/master
| 2023-07-20T19:57:21.121744 | 2021-08-20T05:09:22 | 2021-08-20T05:09:22 | 264,374,548 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 46 |
tst
|
Test2.tst
|
hi this is tst file i want to create and push
|
24da3377e834a1584042db87dae92d0a14c6ffe5
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3574/CH4/EX4.3/EX4_3.sce
|
7669aef3939a6fce747d51807341726edfe6de59
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 2,074 |
sce
|
EX4_3.sce
|
// Example 4.3
// Determine (a) Synchronous speed (b) Slip (c) Rotor impedance (d) Rotor current
// (e) Rotor current if changing the shaft load resulted in 1.24 percenr slip
// (f) Speed for the condition in (e)
// Page No. 146
clc;
clear;
close;
// Given data
fs=60; // Frequency
p=6; // Number of poles
nr=1164; // Rotor speed
Rr=0.10; // Equivalent resistance
Xbr=0.54; // Equivalent reactance
Ebr=150; // Blocked rotor voltage per phase
s1=0.0124; // Percent slip
// (a) Synchronous speed
ns=120*fs/p; // Speed
// (b) Slip
s=(ns-nr)/ns;
// (c) Rotor impedance
Zr=(Rr/s)+%i*Xbr;
// Complex to Polar form...
Zr_Mag=sqrt(real(Zr)^2+imag(Zr)^2); // Magnitude part
Zr_Ang=atan(imag(Zr),real(Zr))*180/%pi; // Angle part
// (d) Rotor current
Ir_Mag=Ebr/Zr_Mag; // Magnitude
Ir_Ang=0-Zr_Ang; // Angle
// (e) Rotor current if changing the shaft load resulted in 1.24 percent slip
Zrnew=Rr/s1+%i*Xbr;
// Complex to Polar form...
Zrnew_Mag=sqrt(real(Zrnew)^2+imag(Zrnew)^2); // Magnitude part
Zrnew_Ang=atan(imag(Zrnew),real(Zrnew))*180/%pi; // Angle part
Irnew_Mag=Ebr/Zrnew_Mag; // Magnitude
Irnew_Ang=0-Zrnew_Ang; // Angle
// (f) Speed for the condition in (e)
nr=ns*(1-s1);
// Display result on command window
printf("\n Synchronous speed = %0.0f r/min ",ns);
printf("\n Slip = %0.3f ",s);
printf("\n Rotor impedance magnitude = %0.2f Ohm ",Zr_Mag);
printf("\n Rotor impedance angle = %0.2f deg ",Zr_Ang);
printf("\n Rotor current magnitude = %0.1f Ohm ",Ir_Mag);
printf("\n Rotor current angle = %0.1f deg ",Ir_Ang);
printf("\n Rotor current magnitude by changing the shaft load = %0.1f Ohm ",Irnew_Mag);
printf("\n Rotor current angle by changing the shaft load = %0.2f deg ",Irnew_Ang);
printf("\n New rotor speed = %0.0f r/min ",nr);
|
e35b099427a9e4d7e9299f74c5a734aea40ffdc2
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3647/CH4/EX4.4/ex4_4.sce
|
287dd92df6d95ae37c6be2e31905c9c154ebd2a0
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 388 |
sce
|
ex4_4.sce
|
//Solutions to Problems In applied mechanics
//A N Gobby
clear all;
clc
//initialisation of variables
w=4//lbf
h=40//lbf/ft
d=2//in
g=32.2//ft/s
//CALCULATIONS
P=(d*%pi)*sqrt(w/(h*g))//sec
V=(d*%pi*d)/(P*12)//ft/s
M=(d*%pi/P)^2*(d/12)//ft/s
//RESULTS
printf('the period of vibration=% f sec',P)
printf('Maximum veloity=% f ft/s',V)
printf('Maximum acceleration=% f ft/s',M)
|
5fdea2b3a7a7aef6782a56448008e2bfe66ae4e5
|
c85cd177767bb7028f15fecb201143f86b35ae94
|
/pathplan.sce
|
1cc61b6d15b917bf70a4c055ac45669bc007f1c2
|
[] |
no_license
|
Neucrede/Dummy
|
c879b8b8f2e32da33d53576ce4f56b4638da7df7
|
7f3f158c78620d66abd089dca658297fac0da069
|
refs/heads/master
| 2021-06-18T00:47:59.632096 | 2021-03-31T09:19:08 | 2021-03-31T09:19:08 | 179,017,060 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 2,716 |
sce
|
pathplan.sce
|
function plot_stencil(d)
scf();
a = gca();
// [xmin,ymin; xmax,ymax]
a.data_bounds = [ min(d(1,:))-2, min(d(2,:))-2;
max(d(1,:))+2, max(d(2,:))+2 ];
plot(d(1,:), d(2,:), 'O');
yy = unique(d(2,:));
yy = yy(:)'; // now, yy is a row vector
X = repmat([min(d(1,:))-2; max(d(1,:))+2], 1, length(yy));
Y = repmat(yy, 2, 1);
plot(X, Y, 'blue');
endfunction
function out = unfold(d, n, min_gap)
batches = [];
y_group = gsort(unique(d(2,:)), 'g', 'i');
y_weight = [];
for i = 1 : length(y_group)
y_weight = [y_weight, length(find(d(2,:) == y_group(i)))];
end
out = [];
endfunction
function out = sort_by_y_coord(d)
d_swapped = [d(2,:); d(1,:)];
d_swap_and_sorted = gsort(d_swapped, 'lc', 'i');
d_sorted = [d_swap_and_sorted(2,:); d_swap_and_sorted(1,:)];
out = d_sorted;
endfunction
function out = find_y_interval_of_adjacent_y_groups(d)
d_sorted_by_y_coord = sort_by_y_coord(d);
y1 = d_sorted_by_y_coord(2,:);
if length(y1) < 2 then
out = [];
return;
end
y1 = unique(y1);
y2 = [y1(2:$), 0];
y_diff = [y2; (y2 - y1)];
y_diff(:, find(y_diff(2,:) <= 0)) = [];
out = y_diff;
endfunction
function out = penalty(s, y, w_total, w_avg, w, a, b, c)
out = a * abs(y - s) + b * (w_total + w - w_avg) + c;
endfunction
function out = pp(d, m, min_gap, l)
y = gsort(unique(d(2,:)), 'g', 'i');
// number of distinct y values
n = length(y);
// weight vector
w = [];
for i = 1 : n
w = [w, length(find(d(2,:) == y(i)))];
end
// range of movement of tip number i under the situation that all other
// tips been moved to both ends of the rack.
limits = [];
for i = 1 : m
limits = [limits; (i - 1) * min_gap, l - ((m - i) * min_gap)];
end
mprintf("limits: \n %e \n\n", limits);
dp = list();
wtotal = list();
for i = 1 : n
dp_i = list();
wtotal_i = list();
for j = 1 : m
A_j = zeros(n, n);
next = find(y > limits(j,1) && y < limits(j,2));
mprintf("available next(j=%d): \n %d \n\n", j, next);
for r = 1 : n
p = [next; %nan * ones(next)];
for s = next
if ()
end
end
dp_i(j) = A_j;
end
dp(i) = dp_i;
wtotal(i) = wtotal_i;
end
out = [];
endfunction
|
c5a809d59f5a03e03d7524c2fe7727ee32660b5f
|
01ecab2f6eeeff384acae2c4861aa9ad1b3f6861
|
/xcos_blocks/Hyst_diff_c.sci
|
49e0710079adc6ea9469f62373915c8f05e2725b
|
[] |
no_license
|
jhasler/rasp30
|
9a7c2431d56c879a18b50c2d43e487d413ceccb0
|
3612de44eaa10babd7298d2e0a7cddf4a4b761f6
|
refs/heads/master
| 2023-05-25T08:21:31.003675 | 2023-05-11T16:19:59 | 2023-05-11T16:19:59 | 62,917,238 | 3 | 3 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,926 |
sci
|
Hyst_diff_c.sci
|
global Ut_sim Kappa_sim;
function block=Hyst_diff_c(block,flag)
//disp(flag)
if flag==1
in_out_num = block.ipar(1); //Vectorized
row_vec_io = 1:in_out_num; // Row vector for input & output
block.outptr(1)(row_vec_io)=block.x(2*row_vec_io); //Output
elseif flag==0
in_out_num = block.ipar(1); //Vectorized
row_vec_io = 1:in_out_num; // Row vector for input & output
Cout=1e-12;
C=100e-15;
Ibias=block.rpar(row_vec_io)
block.xd(2*row_vec_io)=(Ibias./Cout).*tanh((Kappa_sim*(block.inptr(1)(row_vec_io)- block.x(2*row_vec_io-1)))/(2*Ut_sim));
//OTA computation
Ioffp=0;
Ioffn=0;
Voffp=0;
Voffn=0;
V1=block.inptr(1)(row_vec_io);
V2=block.x(2*row_vec_io-1)
m_tanh=tanh((Kappa_sim/(2*Ut_sim))*(V1-V2))
I1=Ibias*(0.5+0.5*m_tanh+Voffp)+Ioffp;
I2=Ibias*(0.5-0.5*m_tanh+Voffn)+Ioffn;
sig=1e-4;
Vdd=2.5
Iout=(-I1*(exp(-sig*block.x(2*row_vec_io) /Ut_sim))*(1-exp(-(Vdd-block.x(2*row_vec_io) )/Ut_sim)))+(I2*(exp(-sig*(Vdd-block.x(2*row_vec_io))/Ut_sim))*(1-exp(-block.x(2*row_vec_io)/Ut_sim)));
//
//disp(Iout)
block.xd(2*row_vec_io) =- Iout/Cout;
//
Isatn=53.58e-9;
Isatp=110e-9;
sigma=5e-2
Vtp=0.866;
Vtn= 0.313;
Inmos=Isatn * log(1 + exp((Kappa_sim*(block.x(2*row_vec_io)-Vtn) - block.x(2*row_vec_io-1) + sigma*2.5)/Ut_sim ))^2 - Isatn * log(1 + exp((Kappa_sim*(block.x(2*row_vec_io)-Vtn) + sigma*block.x(2*row_vec_io-1) - 2.5)/Ut_sim ))^2
Ipmos=Isatp * log(1 + exp((Kappa_sim*(2.5 - block.x(2*row_vec_io)-Vtp) - (2.5 - block.x(2*row_vec_io-1)) + sigma*2.5)/Ut_sim ))^2 -Isatp * log(1 + exp((Kappa_sim*(2.5 - block.x(2*row_vec_io)-Vtp) +sigma* (2.5 - block.x(2*row_vec_io-1)) - 2.5)/Ut_sim ))^2
Iout1=Inmos - Ipmos;
block.xd(2*row_vec_io-1)=Iout1./C;//Vc of the hyst diff
end
endfunction
|
37c05dad6958a8b83918173639af7c7bc9624bf8
|
c9cea368728effc50ef3a05f10679bcc5c63382a
|
/Punto1_Parcial.sce
|
1a72f7b749b88d6c0fd18f5315b4dba6cb7c2cbc
|
[] |
no_license
|
juancllanos/Optimizacion
|
dbb30315da1b6b3bfac0d1ace5d8e468557565d3
|
ef85b725af392290dd46febc839f27944a5ed9d7
|
refs/heads/master
| 2020-04-28T05:46:38.128903 | 2019-05-21T21:59:16 | 2019-05-21T21:59:16 | 175,032,693 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 2,204 |
sce
|
Punto1_Parcial.sce
|
// PARCIAL
// (1)
/*
function f = fx(x)
f = 4*x(1) + 4*x(2) - 2*x(3)
disp(-7*x(1)+10*x(2)+2*x(3))
disp(-7*x(1)+10*x(2)+2*x(3) >= 59)
disp(-4*x(1)+7*x(2)+2*x(3))
disp(-4*x(1)+7*x(2)+2*x(3) >= 47)
disp(2*x(1)-3*x(2)-1*x(3))
disp(2*x(1)-3*x(2)-1*x(3) >= -21)
disp(16*x(1)-25*x(2)-5*x(3))
disp(16*x(1)-25*x(2)-5*x(3) >= -155)
endfunction
function f = fy(x)
f = 59*x(1) + 47*x(2) - 21*x(3)- 155*x(4)
disp(-7*x(1) - 4*x(2) + 2*x(3) + 16*x(4))
disp(-7*x(1) - 4*x(2) + 2*x(3) + 16*x(4) <= 4)
disp(10*x(1) + 7*x(2) - 3*x(3) - 25*x(4))
disp(10*x(1) + 7*x(2) - 3*x(3) - 25*x(4) <= 4)
disp(2*x(1) + 2*x(2) - 1*x(3) -5*x(4))
disp(2*x(1) + 2*x(2) - 1*x(3) -5*x(4) <= -2)
endfunction
x = [0 ; 5 ; 6]
y = [0 ; 10 ; 22 ; 0]
fx = fx(x)
disp('----------------')
fy = fy(y)
disp(fy,'f(y)',fx,'f(x)')
*/
// (2)
function y = f3x(x)
y = x(1)**2 + x(2)**2 + x(3)**2 + 6*x(1)*x(2) +4*x(1)*x(3)+8*x(2)*x(3) -12*x(1)-4*x(2) - 2*x(3)
//disp(x,'Este x')
//disp(x(1)<=1.5)
//disp(x(2)<=1.5)
//disp(x(3)<=1.5)
//disp(x(2) + x(3) ==2)
endfunction
x3 = [1.5 ; 1 ; 1]
q = f3x(x3)
disp(q,'f(x)')
gr = numderivative (f3x,x3)'
disp(gr,'gr')
o = [0 1 0]
z = -o'\gr
disp(z,'u')
disp(z*o'+gr,'sol total')
// (3)
/*
function y = fx(x)
disp(x,'Para x = ')
y = (x(1)-6)**4 + 2*(x(1)+x(2)-13)**2
disp(x(1)+x(2) == 10)
disp(x(1) >= 4)
disp(x(2) >= 0)
endfunction
x1 = [4 ; 6]
x2 = [5 ; 5]
f1 = fx(x1)
f2 = fx(x2)
disp(f2,'f(x2)',f1,'f(x1)')
x = [6 ; 7]
//grx = numderivative(fx,x)
//disp(grx,'grx')
grx1 = numderivative(fx,x1)'
grx2 = numderivative(fx,x2)'
disp(grx2,'grx2',grx1,'grx1')
a = [1 0 1; 0 1 1]
sol1 = -a\grx1
u11 = sol1(1)
u21 = sol1(2)
v11 = sol1(3)
disp(v11,'v11',u21,'u2',u11,'u1')
sol2 = -a\grx2
u12 = sol2(1)
u22 = sol2(2)
v12 = sol2(3)
disp(v12,'v12',u22,'u2',u12,'u1')
disp(sol2,'kkt x2',sol1,'kkt x1')
disp('---------------------------------------------')
kktx1 = grx1 + u11*[1;0] + u21 * [0;1] + v11*[1;1]
kktx2 = grx2 + u12*[1;0] + u22 * [0;1] + v12*[1;1]
disp(kktx2,'kktx2',kktx1,'kktx1')
*/
|
8839cdebbd2d643506dc5a3f9a16631ce0a18a3d
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/32/CH5/EX5.10/5_10.sce
|
d494706638efebe25494ac91ecca62b11467054a
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 500 |
sce
|
5_10.sce
|
//pathname=get_absolute_file_path('5.10.sce')
//filename=pathname+filesep()+'5.10-data.sci'
//exec(filename)
//Initial pressure(in kPa):
p1=3000
//Initial volume(in m^3):
v1=0.05
//Final volume(in m^3):
v2=0.3
//Value of n:
n=1.4
//Final pressure(in MPa):
p2=p1*((v1/v2)^n)
//Entropy change:
dS=0
//Change in enthalpy(in kJ):
dH=((p1*(v1^n))^(1/n))*(p1^((n-1)/n)-p2^((n-1)/n))/((n-1)/n)
printf("\nRESULT\n")
printf("\nEnthalpy change = %f kJ",dH)
printf("\nEntropy change = %d",dS)
|
ab72f42781807420a1eb5261a9027edc4c52d899
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2258/CH1/EX1.1/1_1.sce
|
55062a1694b5a4f1a8cbac53bf9c50c85408c996
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 308 |
sce
|
1_1.sce
|
clc();
clear;
// To calculate the de Broglie wavelength
c=3*10^8; //velocity of light in m/s
v=c/10; //velocity of proton in m/s
m=1.67*10^(-27); //mass of proton in kg
h=6.626*10^(-34);
lamda=h/(m*v); //de Broglie wavelength
printf("The de Broglie wavelength in metres is");
disp(lamda);
|
2a740817bde82e8a5c0d5d217241012118d6031a
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/226/CH3/EX3.14/example14_sce.sce
|
f845eb620e39112670c54dd3eacb62ba60e98644
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 280 |
sce
|
example14_sce.sce
|
//chapter 3
//example 3.14
//page 101
printf("\n")
printf("given")
Edc=20;vo=.24;Vo=20;Il=40*10^-3;fr=120;
Eomax=(3.14*Edc)/2
Epeak=(4*Eomax)/(3*3.14)
vi=Epeak;
Rl=Vo/Il
Xlc=(2*Rl)/3
Lc=Xlc/(2*3.14*fr)
L=1.25*Lc;
Xl=2*3.14*fr*L
Xc=Xl/((vi/vo)+1)
C1=1/(2*3.14*fr*Xc)
|
fd2b54c53ab6cc871eb76e5e4087daec36b86eba
|
8aff21ee3944bdacbff38a386556c89c38377c6a
|
/augstate.sci
|
09eb66d9c168e6de343da15ec09644dd1a3a1e01
|
[] |
no_license
|
rutup1595/control-system
|
bd4704a4aa437a66260301a22adb5e55b49c5c84
|
b30d559d8835cd278cc6d6bb81f821cdfcc9ee55
|
refs/heads/master
| 2021-01-17T10:17:03.192056 | 2019-10-10T05:28:46 | 2019-10-10T05:28:46 | 59,283,553 | 0 | 1 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 2,320 |
sci
|
augstate.sci
|
function[]=augstate(sys)
//
//Calling Sequence
//function[]=augstate(sys)
//Parameters
//sys- SISO or MIMO state space models
//Description
//augstate function appends states to the outputs of a state-space model
//this command is useful to close the loop on a full-state feedback gain u = Kx. After preparing the plant with augstate,you can use the FEEDBACK command to derive the closed-loop model.
// augstate function is not defined for array of SISO.
//Examples:
// 1.aa=syslin('c',[1,3;4,5],[6;8],[2,3],[1]);
// a1=augstate(aa)
// 2.ab=syslin('c',[1,2;3,4],[4,5;6,7],[8,9;0,1],[1,0;0,5])
// a2=augstate(ab)
//See also
// siso ,mimo
//Authors
//Rutuja Moharil
//Bibliography
//http://www-rohan.sdsu.edu/doc/matlab/toolbox/control/ref/augstate.html
//http://octave.sourceforge.net/control/function/augstate.html
select typeof(sys)
case "state-space" then // check if the entered system is state space model
[A B C D]=abcd(sys); // extracting A,B,C,D matrices
t=mtlb_size(A);
[row,col]=size(B);
if (isempty(C)==%t) then
C=zeros(size(A,1),size(A,2));
end
if(isempty(D)==%t) then
D=zeros(size(C,1),size(B,2));
end
C=cat(1,C,eye(t,t)) // cocatenation of matrix C and identity matrix of size of A
D=cat(1,D,zeros(t,col)) // cocatenation of matrix A and null matrix of row of A and column of D
if sys.dt=='c' then
sysa=syslin('c',A,B,C,D);
disp(sysa)
else
if sys.dt=='d' then
dt=1
else
dt=sys.dt
end
sysa=syslin('d',A,B,C,D);
disp(sysa)
disp (dt,"Sample time :")
end
else // for any other system display the error
error(msprintf(_("\n %s: Wrong type of input argument #%d: State space model expected.\n"),"augstate",1))
end;
endfunction
|
93d0cdc2646680a66481ec0bc7a585f00286607b
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1616/CH2/EX2.22/ex2_22.sce
|
48119fe7e784f4f29504abe040f374640d84708a
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 317 |
sce
|
ex2_22.sce
|
//ex2.22 Design the transmission line section as areactive element
f=6e9;
w=2*%pi*f;
L=0.01e-6;
X=w*L;
Z0=150;
lamda=4.0;
b=2*%pi/lamda;
loc=(1/b)*acot(-X/Z0); //length of the line
disp('The reactance to be realized is '+string(X)+' ohm');
disp('The length of the line therefore is = '+string(loc)+' cm');
|
b5404f03ce5c4ca8122c8af9fd63c9d5f0cb0cd8
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3647/CH3/EX3.5/ex3_5.sce
|
6198534a2249aadd110be3bac488d6c02b4b4b89
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 349 |
sce
|
ex3_5.sce
|
//Solutions to Problems In applied mechanics
//A N Gobby
clear all;
clc
//initialisation of variables
w=3//lbf
v=5//ft
a=60//degree
g=32.2//ft
u=28.4//ft/s
t=25.4//ft/s
q=12//ft
p=1.5//ft
//CALCULATIONS
U=sqrt(g*v)//ft/s
T=w*(t)^2/(2*g)+w*cosd(a)//lbf
W=q+p//lbf
//RESULTS
printf('the tension in the string at position C=% f lbf',W)
|
ee576634e3cee002c70033ba7351e66361b4603b
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/995/CH9/EX9.2/Ex9_2.sce
|
e05f7a0722d1b3ade7b5e06756d0d49e0c72635b
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 238 |
sce
|
Ex9_2.sce
|
//Ex:9.2
clc;
clear;
close;
r1=1000;
r2=1000;
c=100*10^-9;
f=(1/(2*%pi*c*r1));
printf("The freq of oscillation at 1 kohm= %f Hz",f);
R1=6000;
R2=6000;
F=(1/(2*%pi*c*R1));
printf("\nThe freq of oscillation at 6 kohm= %f Hz",F);
|
b14a8c9a74a4e5da4648c90c27627ff4951971c1
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3161/CH14/EX14.1/Ex14_1.sce
|
f7784bcdb63400192012c38e9edaf478b4adc4fb
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 998 |
sce
|
Ex14_1.sce
|
clc;
//page 738
//problem 14.1
//Boltzman constant k = 1.3806488 × 10-23 m2 kg s-2 K-1
k = 1.3806488 * 10^-23;
//Let room temperature be 27 C
T = 27 + 273;
//Bandwidth BW = 10 MHz
BW = 10 * 10 ^6;
//For (a)
//Let the equivalent resistance be Ra
Ra = 10 + 10;
//RMS Noise Voltage be Va
Va = (4*k*T*Ra*BW)^0.5;
disp('The rms voltage at output a is '+string(Va)+' Volt');
//For (b)
//Let the equivalent resistance be Rb
Rb = (10 * 10)/(10+10);
//RMS Noise Voltage be Vb
Vb = (4*k*T*Rb*BW)^0.5;
disp('The rms voltage at output b is '+string(Vb)+' Volt');
//For (c)
Rc = 10;
C = 1*10^-9;
//In the textbook, the author has forgotten to multiply the result with T, hence has obtained an erroneous result.
//The given answer is 28.01uV but the correct answer is found out to be 1.2uV
Vc_square = 2*k*integrate('Rc/(1 + (2*%pi*Rc*C*f)^2)','f',-10^7,10^7);
Vc = Vc_square^0.5;
disp('The rms voltage at output c is '+string(Vc)+' Volt');
|
816d21431aec1e022077ac542f62d0079d3e20e6
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3871/CH6/EX6.27/Ex6_27.sce
|
82d173d3cd47a12229ecb5dc0ed20ba4672b1f28
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 590 |
sce
|
Ex6_27.sce
|
//===========================================================================
//chapter 6 example 27
clc;
clear all;
//variable declaration
KT = 198; //turn ratio
e =0; //ratio error
Is = 5; // secondary current in A
P = 5; //load in VA
Rs = 0.02; //resistance in Ω
KN = 200; //KN=KC since e=0
KC = 200;
//calculations
V2 = P/Is; //secondary voltage in V
Es = V2+(Is*Rs); //secondary induced emf in V
Ep = Es/KT; //primary induced emf
Ie = (KC-KT)*Is; //eddy current loss in A
IL = Ep*Ie; //iron loss in W
//result
mprintf("iron loss = %3.3f mW",(IL*10^3));
|
c5aa5a7b00887c97a25bf0a39dda9493f91cba40
|
99b4e2e61348ee847a78faf6eee6d345fde36028
|
/Toolbox Test/cell2sos/cell2sos1.sce
|
09357dd68282974998e4221f1bbd61a2980b8fb0
|
[] |
no_license
|
deecube/fosseetesting
|
ce66f691121021fa2f3474497397cded9d57658c
|
e353f1c03b0c0ef43abf44873e5e477b6adb6c7e
|
refs/heads/master
| 2021-01-20T11:34:43.535019 | 2016-09-27T05:12:48 | 2016-09-27T05:12:48 | 59,456,386 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 395 |
sce
|
cell2sos1.sce
|
//i/p is a 1X4 cell
c=cell(1,4);
c(1,1).entries=[0.3209,0.5183,0.3209];
c(1,2).entries=[1,0.1677,0.2575];
c(1,3).entries=[1,0.8927,1];
c(1,4).entries=[1,0.6196,0.8747];
sos=cell2sos(c);
disp(sos);
//output
//column 1 to 4
//
// 0.3209 0.5183 0.3209 1.
// 1. 0.8927 1. 1.
//
// column 5 to 6
//
// 0.1677 0.2575
// 0.6196 0.8747
//
|
dd19b0dc378d4e1b28abf8c53f504ee9f8d978fc
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3769/CH8/EX8.4/Ex8_4.sce
|
f3d2ee70202c5dcc5b696366809dd0144ddf883a
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 308 |
sce
|
Ex8_4.sce
|
clear
//Given
a=60 //degree
u=4*3.14*10**-7 //T/A m
Bc=2
//Calculation
//
a=(Bc/2.0)/(tan(60)*180/3.14)
B1=(10**-7*tan(60)*(sin(60*180/3.14)+sin(60*180/3.14)))*10
B=3*B1
//Result
printf("\n Magnetic fieldat the centroid of the triangle is %0.0f *10**-7 T",B*10**7)
|
276a0f7aa51e576de86ac9045d699bf0e2ee9fa3
|
ad617742f184bf6d4cceb3e9c99232d8bd52b862
|
/tests/3211.tst
|
73da903b4cf89fe4a7d4da6a97d602be60f2bcee
|
[
"LicenseRef-scancode-unknown-license-reference",
"LicenseRef-scancode-other-permissive",
"BSD-2-Clause"
] |
permissive
|
9track/hyperion
|
d621343e7eea27c45db49c7c284dd1680491c82c
|
9ceed2cc7261820eef01c55dac9b9a6ae47636b2
|
refs/heads/master
| 2022-09-15T12:19:09.059528 | 2020-05-28T03:05:29 | 2020-05-28T03:05:29 | 268,044,749 | 3 | 1 |
NOASSERTION
| 2020-05-30T09:03:56 | 2020-05-30T09:03:55 | null |
UTF-8
|
Scilab
| false | false | 6,975 |
tst
|
3211.tst
|
#----------------------------------------------------------
# In addition to the below 3211.core file this test
# also uses an associated "3211.rexx" script as well.
#----------------------------------------------------------
*If \$rexx_supported
*Message SKIPPING: Testcase 3211 printer
*Message REASON: No Hercules Rexx support.
*Else
*If $rexx_VERSION = ''
*Message SKIPPING: Testcase 3211 printer
*Message REASON: Rexx is not installed.
*Else
*If $rexx_package = 'Regina'
*Testcase 3211 printer (Regina)
# Prepare test environment
mainsize 1
numcpu 1
sysclear
archlvl 390
loadcore "$(testpath)/3211.core"
detach 00f
attach 00f 3211 "3211.txt"
diag8cmd enable noecho # need diag8 to exec rexx script
shcmdopt enable diag8 # rexx script needs shell access
# Set needed Hercules Rexx processing options
rexx mode subroutine msglevel off msgprefix off errprefix off resolver on syspath on extensions .rexx start auto
#---------------------------------------------------
# Define the tests we want to be run
# Skip tests 3, 4 and 9 because Regina Rexx sucks.
#---------------------------------------------------
r ff0=00000000000000000000000000000000 # (start with none)
r ff0=00f1f20000f5f6f7f800000000000000 # (skip 3, 4 and 9)
# Run the tests...
runtest 0.1 # (plenty of time)
# Clean up afterwards
detach 000f # (no longer needed)
diag8cmd disable noecho # (no longer needed)
shcmdopt disable nodiag8 # (no longer needed)
*Compare
r 1000.10
*Want "Return Code flags" 00000000 00000000 00000000 00000000
*Done
*Else
*If $rexx_SOURCE = 'DARWIN'
*Testcase 3211 printer (Apple)
# Prepare test environment
mainsize 1
numcpu 1
sysclear
archlvl 390
loadcore "$(testpath)/3211.core"
detach 00f
attach 00f 3211 "3211.txt"
diag8cmd enable noecho # need diag8 to exec rexx script
shcmdopt enable diag8 # rexx script needs shell access
# Set needed Hercules Rexx processing options
rexx mode subroutine msglevel off msgprefix off errprefix off resolver on syspath on extensions .rexx start auto
#----------------------------------------------------------
# Define the tests we want to be run
# Skip tests 3, 4 and 9 because the only OORexx available
# for Apple Mac is OORexx 5.0, and it apparently has the
# same or similar Rexx bug as Regina! (i.e. for reasons
# that are unknown tests 3, 4 and 9 seem to always fail)
#----------------------------------------------------------
r ff0=00000000000000000000000000000000 # (start with none)
r ff0=00f1f20000f5f6f7f800000000000000 # (skip 3, 4 and 9)
# Run the tests...
runtest 0.1 # (plenty of time)
# Clean up afterwards
detach 000f # (no longer needed)
diag8cmd disable noecho # (no longer needed)
shcmdopt disable nodiag8 # (no longer needed)
*Compare
r 1000.10
*Want "Return Code flags" 00000000 00000000 00000000 00000000
*Done
*Else
*Testcase 3211 printer (OORexx)
# Prepare test environment
mainsize 1
numcpu 1
sysclear
archlvl 390
loadcore "$(testpath)/3211.core"
detach 00f
attach 00f 3211 "3211.txt"
diag8cmd enable noecho # need diag8 to exec rexx script
shcmdopt enable diag8 # rexx script needs shell access
# Set needed Hercules Rexx processing options
rexx mode subroutine msglevel off msgprefix off errprefix off resolver on syspath on extensions .rexx start auto
# Define the tests we want to be run
r ff0=00000000000000000000000000000000 # (start with none)
r ff0=00f1f2f3f4f5f6f7f8f9000000000000 # (default = all)
# Run the tests...
runtest 0.1 # (plenty of time)
# Clean up afterwards
detach 000f # (no longer needed)
diag8cmd disable noecho # (no longer needed)
shcmdopt disable nodiag8 # (no longer needed)
*Explain
*Explain If the above is an "unexpected wait state" of 000100D8
*Explain it means that the DIAG8 instruction completed with a non-
*Explain zero condition code. The likely reason for this is the
*Explain results buffer wasn't large enough because the Hercules
*Explain command the test issued resulted in an unexpected error
*Explain message (which couldn't fit into DIAG8's response buffer).
*Explain
*Explain If any of the below test completion flags are non-zero
*Explain it means that particular test has failed. For example,
*Explain if the completion flags are 000000F3 F4F5F6F7 F8F90000...
*Explain it means that tests 3 thru 9 have failed (F3 = '3' etc).
*Explain
*Compare
r 1000.10
*Want "Return Code flags" 00000000 00000000 00000000 00000000
* *************************************************
* The following should all have valid file sizes.
* (i.e. they should all be numbers, e.g. 38, etc)
* If they are not numbers (e.g. still "aa"), then
* it means the Rexx being used is SEVERLY BROKEN!
* *************************************************
*
* Test 03 sizes should be the same
* Test 04 " " " DIFFERENT
* Test 09 " " " the same
*
* *************************************************
r 2100.100 # SIZ03A (before)
r 2200.100 # SIZ03B (after) should be SAME
* *************************************************
r 2300.100 # SIZ04A (before)
r 2400.100 # SIZ04B (after) should be DIFFERENT
* *************************************************
r 2500.100 # SIZ09A (before)
r 2600.100 # SIZ09B (after) should be SAME
* *************************************************
*Done
*Fi
*Fi
*Fi
*Fi
|
d102a116736e43c9972ffa5efee487fd06b16823
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1271/CH19/EX19.7/example19_7.sce
|
30e2e78302d05d82288de9c01a0c6d88aa4bbd0f
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 395 |
sce
|
example19_7.sce
|
clc
// Given that
w = 26.91 // isotopic mass of superconducting sample
Tc = 1.19 // first critical temperature in K
w_ = 32.13 // increased isotope mass of superconducting sample
// Sample Problem 7 on page no. 19.16
printf("\n # PROBLEM 7 # \n")
printf("Standard formula used \n ")
printf(" T_c*M^(1/2) = constant \n")
Tc_ = Tc * (w / w_)^(1/2)
printf("\n Critical temperature is %f K.",Tc_)
|
8f37b93d028d8f67889016055df6bbc413fd1fb2
|
e04f3a1f9e98fd043a65910a1d4e52bdfff0d6e4
|
/New LSTMAttn Model/.data/lemma-split/GOLD-TEST/ood.tst
|
2a69249a0b66389c2da0d483bba333b085e3fb06
|
[] |
no_license
|
davidgu13/Lemma-vs-Form-Splits
|
c154f1c0c7b84ba5b325b17507012d41b9ad5cfe
|
3cce087f756420523f5a14234d02482452a7bfa5
|
refs/heads/master
| 2023-08-01T16:15:52.417307 | 2021-09-14T20:19:28 | 2021-09-14T20:19:28 | 395,023,433 | 3 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 10,359 |
tst
|
ood.tst
|
ko:ji ko:ji N;SG
ko:ji kokji N;PL
cihil cihil N;SG
cihil cihil N;PL
si:l si:l N;PL
si:l si:l N;SG
baʼa baʼad V;IPFV;SG;FUT
baʼa ba: V;PRF;SG;PRS
baʼa baʼad V;IPFV;PL;FUT
baʼa ba'iñ V;IMP;PL;PRS
baʼa baʼa V;IPFV;SG;PRS
baʼa baʼa V;IPFV;PL;PRS
baʼa ba: V;PRF;PL;PRS
baʼa ba'iñ V;IMP;SG;PRS
ha:hag ha:hag N;SG
ha:hag ha:hag N;PL
kotoñ kotoñ N;SG
kotoñ koktoñ N;PL
naw naw N;PL
naw naw N;SG
s-da:pk s-dadpkad V;IPFV;PL;FUT
s-da:pk s-dadpkiñ V;IMP;PL;PRS
s-da:pk s-dadpk V;IPFV;PL;PRS
s-da:pk s-da:pkiñ V;IMP;SG;PRS
s-da:pk s-da:pkad V;IPFV;SG;FUT
s-da:pk s-da:pk V;IPFV;SG;PRS
wu:s̥ad wu:s̥adad V;IPFV;SG;FUT
wu:s̥ad wu:s̥a V;PRF;SG;PRS
wu:s̥ad wu:s̥a V;PRF;PL;PRS
wu:s̥ad wu:s̥ad V;IPFV;SG;PRS
wu:s̥ad wu:s̥ad V;IPFV;PL;PRS
wu:s̥ad wu:s̥adiñ V;IMP;PL;PRS
wu:s̥ad wu:s̥adiñ V;IMP;SG;PRS
wu:s̥ad wu:s̥adad V;IPFV;PL;FUT
siswuimad siswuimad V;IPFV;SG;PRS
siswuimad siswuimadiñ V;IMP;PL;PRS
siswuimad siswuimadiñ V;IMP;SG;PRS
siswuimad siswuimad V;PRF;SG;PRS
siswuimad siswuimadad V;IPFV;PL;FUT
siswuimad siswuimad V;PRF;PL;PRS
siswuimad siswuimad V;IPFV;PL;PRS
siswuimad siswuimadad V;IPFV;SG;FUT
ʼu:gk ʼu:gkiñ V;IMP;SG;PRS
ʼu:gk ʼuʼugkiñ V;IMP;PL;PRS
ʼu:gk ʼu:gk V;IPFV;SG;PRS
ʼu:gk ʼuʼugk V;IPFV;PL;PRS
ʼu:gk ʼu:gkad V;IPFV;SG;FUT
ʼu:gk ʼuʼugkad V;IPFV;PL;FUT
wosonakud̥ wosonakud̥ N;SG
wosonakud̥ wopsonakud̥ N;PL
ceposid cecposid V;IPFV;PL;PRS
ceposid cepos V;PRF;SG;PRS
ceposid ceposidad V;IPFV;SG;FUT
ceposid cecposidad V;IPFV;PL;FUT
ceposid ceposid V;IPFV;SG;PRS
ceposid ceposidiñ V;IMP;SG;PRS
ceposid cecposidiñ V;IMP;PL;PRS
ceposid cecpos V;PRF;PL;PRS
s-muʼuk s-muʼuk V;IPFV;SG;PRS
s-muʼuk s-muʼukad V;IPFV;SG;FUT
s-muʼuk s-muʼumkiñ V;IMP;PL;PRS
s-muʼuk s-muʼukiñ V;IMP;SG;PRS
s-muʼuk s-muʼumkad V;IPFV;PL;FUT
s-muʼuk s-muʼumk V;IPFV;PL;PRS
tas̥ga tas̥ga N;SG
tas̥ga tas̥ga N;PL
ʼi:bhĕ ʼi:bhĕ V;PRF;SG;PRS
ʼi:bhĕ ʼi:bhed V;IPFV;SG;FUT
ʼi:bhĕ ʼi:bhĕ V;PRF;PL;PRS
ʼi:bhĕ ʼi:bhed V;IPFV;PL;FUT
ʼi:bhĕ ʼi:bheñ V;IMP;PL;PRS
ʼi:bhĕ ʼi:bheñ V;IMP;SG;PRS
ʼi:bhĕ ʼi:bhĕ V;IPFV;PL;PRS
ʼi:bhĕ ʼi:bhĕ V;IPFV;SG;PRS
hewek hewekiñ V;IMP;SG;PRS
hewek hewek V;PRF;SG;PRS
hewek hewek V;IPFV;SG;PRS
hewek hewek V;IPFV;PL;PRS
hewek hewekiñ V;IMP;PL;PRS
hewek hewek V;PRF;PL;PRS
hewek hewekad V;IPFV;PL;FUT
hewek hewekad V;IPFV;SG;FUT
kahon kahon N;SG
kahon kakhon N;PL
ceoj ceoj N;SG
ceoj cecoj N;PL
s-wohocid s-wohocidiñ V;IMP;SG;PRS
s-wohocid s-wohoc V;PRF;PL;PRS
s-wohocid s-wohocidiñ V;IMP;PL;PRS
s-wohocid s-wohocid V;IPFV;PL;PRS
s-wohocid s-wohocidad V;IPFV;SG;FUT
s-wohocid s-wohocid V;IPFV;SG;PRS
s-wohocid s-wohoc V;PRF;SG;PRS
s-wohocid s-wohocidad V;IPFV;PL;FUT
s-ape s-apeñ V;IMP;PL;PRS
s-ape s-aped V;IPFV;SG;FUT
s-ape s-apeñ V;IMP;SG;PRS
s-ape s-aped V;IPFV;PL;FUT
s-ape s-ape V;IPFV;PL;PRS
s-ape s-ape V;IPFV;SG;PRS
cicwi cicwi V;PRF;SG;PRS
cicwi cicwiñ V;IMP;SG;PRS
cicwi cicwi V;PRF;PL;PRS
cicwi cicwid V;IPFV;PL;FUT
cicwi cicwi V;IPFV;SG;PRS
cicwi cicwid V;IPFV;SG;FUT
cicwi cicwi V;IPFV;PL;PRS
cicwi cicwiñ V;IMP;PL;PRS
si:s̥p si:s̥p V;IPFV;SG;PRS
si:s̥p si:s̥piñ V;IMP;SG;PRS
si:s̥p sisis̥p V;IPFV;PL;PRS
si:s̥p si:s̥pad V;IPFV;SG;FUT
si:s̥p si:s̥ V;PRF;SG;PRS
si:s̥p sisis̥piñ V;IMP;PL;PRS
si:s̥p sisis̥pad V;IPFV;PL;FUT
si:s̥p sisis̥ V;PRF;PL;PRS
ʼod̥pig ʼod̥pĭ V;PRF;SG;PRS
ʼod̥pig ʼod̥pig V;IPFV;SG;PRS
ʼod̥pig ʼoʼod̥pigiñ V;IMP;PL;PRS
ʼod̥pig ʼod̥pigiñ V;IMP;SG;PRS
ʼod̥pig ʼod̥pigad V;IPFV;SG;FUT
ʼod̥pig ʼoʼod̥pigad V;IPFV;PL;FUT
ʼod̥pig ʼoʼod̥pig V;IPFV;PL;PRS
ʼod̥pig ʼoʼod̥pĭ V;PRF;PL;PRS
ʼoʼohana ʼoʼohana N;SG
ʼoʼohana ʼoʼohana N;PL
kud̥ut kud̥utiñ V;IMP;PL;PRS
kud̥ut kud̥utad V;IPFV;PL;FUT
kud̥ut kud̥utad V;IPFV;SG;FUT
kud̥ut kud̥ut V;IPFV;PL;PRS
kud̥ut kud̥utiñ V;IMP;SG;PRS
kud̥ut kud̥ut V;IPFV;SG;PRS
pa:nt papant V;PRF;PL;PRS
pa:nt pa:ntiñ V;IMP;SG;PRS
pa:nt papantiñ V;IMP;PL;PRS
pa:nt papant V;IPFV;PL;PRS
pa:nt pa:ntad V;IPFV;SG;FUT
pa:nt papantad V;IPFV;PL;FUT
pa:nt pa:nt V;IPFV;SG;PRS
pa:nt pa:nt V;PRF;SG;PRS
kawhi kawhi N;PL
kawhi kawhi N;SG
s-iʼowĭ s-iʼowĭ N;PL
s-iʼowĭ s-iʼowĭ N;SG
pisaltakud̥ pipsaltakud̥ N;PL
pisaltakud̥ pisaltakud̥ N;SG
memd̥a memd̥ad V;IPFV;SG;FUT
memd̥a wopoʼod V;IPFV;PL;FUT
memd̥a wopo'iñ V;IMP;PL;PRS
memd̥a memd̥a V;IPFV;SG;PRS
memd̥a wopoʼo V;IPFV;PL;PRS
memd̥a memd̥añ V;IMP;SG;PRS
hu:ñ hu:ñ N;SG
hu:ñ huhuñ N;PL
s-onk s-onkad V;IPFV;SG;FUT
s-onk s-oʼonkiñ V;IMP;PL;PRS
s-onk s-oʼonk V;IPFV;PL;PRS
s-onk s-oʼonkad V;IPFV;PL;FUT
s-onk s-onk V;IPFV;SG;PRS
s-onk s-onkiñ V;IMP;SG;PRS
ʼelid ʼelidad V;IPFV;PL;FUT
ʼelid ʼelĭ V;PRF;PL;PRS
ʼelid ʼelidiñ V;IMP;SG;PRS
ʼelid ʼelidad V;IPFV;SG;FUT
ʼelid ʼelidiñ V;IMP;PL;PRS
ʼelid ʼelid V;IPFV;SG;PRS
ʼelid ʼelĭ V;PRF;SG;PRS
ʼelid ʼelid V;IPFV;PL;PRS
ʼoʼohan ʼoʼohaniñ V;IMP;SG;PRS
ʼoʼohan ʼoʼohanad V;IPFV;SG;FUT
ʼoʼohan ʼoʼoha V;PRF;PL;PRS
ʼoʼohan ʼoʼohaniñ V;IMP;PL;PRS
ʼoʼohan ʼoʼoha V;PRF;SG;PRS
ʼoʼohan ʼoʼohan V;IPFV;SG;PRS
ʼoʼohan ʼoʼohan V;IPFV;PL;PRS
ʼoʼohan ʼoʼohanad V;IPFV;PL;FUT
tapial tatpial N;PL
tapial tapial N;SG
ceʼewidakud̥ ceʼewidakud̥ N;PL
ceʼewidakud̥ ceʼewidakud̥ N;SG
ceʼewid ceʼewi V;PRF;SG;PRS
ceʼewid ceʼewidiñ V;IMP;SG;PRS
ceʼewid ceʼewidad V;IPFV;PL;FUT
ceʼewid ceʼewid V;IPFV;SG;PRS
ceʼewid ceʼewid V;IPFV;PL;PRS
ceʼewid ceʼewidiñ V;IMP;PL;PRS
ceʼewid ceʼewi V;PRF;PL;PRS
ceʼewid ceʼewidad V;IPFV;SG;FUT
hemajkam hemajkam N;SG
hemajkam hehemajkam N;PL
hi:wodag hihwodag N;PL
hi:wodag hi:wodag N;SG
huhuʼid huhuʼidiñ V;IMP;PL;PRS
huhuʼid huhuʼi V;PRF;SG;PRS
huhuʼid huhuʼid V;IPFV;PL;PRS
huhuʼid huhuʼidiñ V;IMP;SG;PRS
huhuʼid huhuʼid V;IPFV;SG;PRS
huhuʼid huhuʼi V;PRF;PL;PRS
huhuʼid huhuʼidad V;IPFV;PL;FUT
huhuʼid huhuʼidad V;IPFV;SG;FUT
koʼokolmad koʼokolmadad V;IPFV;SG;FUT
koʼokolmad koʼokolmadad V;IPFV;PL;FUT
koʼokolmad koʼokolmad V;IPFV;PL;PRS
koʼokolmad koʼokolmad V;PRF;PL;PRS
koʼokolmad koʼokolmadiñ V;IMP;SG;PRS
koʼokolmad koʼokolmadiñ V;IMP;PL;PRS
koʼokolmad koʼokolmad V;PRF;SG;PRS
koʼokolmad koʼokolmad V;IPFV;SG;PRS
tlo:gi tlo:gi N;SG
tlo:gi tlolgi N;PL
cendad cecendad V;IPFV;PL;PRS
cendad cecendad V;PRF;PL;PRS
cendad cecendadiñ V;IMP;PL;PRS
cendad cendad V;IPFV;SG;PRS
cendad cendadiñ V;IMP;SG;PRS
cendad cendad V;PRF;SG;PRS
cendad cecendadad V;IPFV;PL;FUT
cendad cendadad V;IPFV;SG;FUT
gaʼa gaʼañ V;IMP;SG;PRS
gaʼa gaʼad V;IPFV;SG;FUT
gaʼa gaʼad V;IPFV;PL;FUT
gaʼa gai V;PRF;PL;PRS
gaʼa gaʼa V;IPFV;SG;PRS
gaʼa gaʼa V;IPFV;PL;PRS
gaʼa gai V;PRF;SG;PRS
gaʼa gaʼañ V;IMP;PL;PRS
to:nk totonk N;PL
to:nk to:nk N;SG
giʼipig giʼipigad V;IPFV;SG;FUT
giʼipig giʼipig V;IPFV;PL;PRS
giʼipig giʼipig V;IPFV;SG;PRS
giʼipig giʼipigiñ V;IMP;SG;PRS
giʼipig giʼipĭ V;PRF;PL;PRS
giʼipig giʼipĭ V;PRF;SG;PRS
giʼipig giʼipigiñ V;IMP;PL;PRS
giʼipig giʼipigad V;IPFV;PL;FUT
s-wagima s-wapagimañ V;IMP;PL;PRS
s-wagima s-wagima V;IPFV;SG;PRS
s-wagima s-wapagimad V;IPFV;PL;FUT
s-wagima s-wapagima V;IPFV;PL;PRS
s-wagima s-wagimad V;IPFV;SG;FUT
s-wagima s-wagimañ V;IMP;SG;PRS
elpig ʼeʼelpigad V;IPFV;PL;FUT
elpig ʼelpi V;PRF;SG;PRS
elpig elpigad V;IPFV;SG;FUT
elpig ʼeʼelpi V;PRF;PL;PRS
elpig elpigiñ V;IMP;SG;PRS
elpig elpig V;IPFV;SG;PRS
elpig ʼeʼelpigiñ V;IMP;PL;PRS
elpig ʼeʼelpig V;IPFV;PL;PRS
cu:hug cu:hug N;PL
cu:hug cu:hug N;SG
wakonakud̥ wakonakud̥ N;SG
wakonakud̥ wapkonakud̥ N;PL
wopo wopo N;PL
wopo wopo N;SG
mehĭ mehĭ N;SG
mehĭ mehĭ N;PL
ki: ki: N;SG
ki: ki: V;IPFV;PL;PRS
ki: ki:d V;IPFV;PL;FUT
ki: ki:d V;IPFV;SG;FUT
ki: ki: V;IPFV;SG;PRS
ki: ki:ñ V;IMP;SG;PRS
ki: ki:kĭ N;PL
ki: ki:ñ V;IMP;PL;PRS
ki: ki:k N;PL
siʼi si'id V;IPFV;PL;FUT
siʼi si: V;PRF;PL;PRS
siʼi si: V;PRF;SG;PRS
siʼi siʼi V;IPFV;PL;PRS
siʼi si'id V;IPFV;SG;FUT
siʼi siʼi V;IPFV;SG;PRS
siʼi siʼiñ V;IMP;PL;PRS
siʼi siʼiñ V;IMP;SG;PRS
wamigĭ wa:pam V;PRF;PL;PRS
wamigĭ wa:pamgid V;IPFV;PL;FUT
wamigĭ wamigiñ V;IMP;PL;PRS
wamigĭ wamigĭ V;IPFV;SG;PRS
wamigĭ wa:pamgĭ V;IPFV;PL;PRS
wamigĭ wamigiñ V;IMP;SG;PRS
wamigĭ wam V;PRF;SG;PRS
wamigĭ wamigid V;IPFV;SG;FUT
huc huc N;SG
huc huhuc N;PL
Tohono ʼOʼodham Tohono ʼOʼodham N;SG
Tohono ʼOʼodham Tohono ʼOʼodham N;PL
ʼoimed̥ ʼoimed̥ad V;IPFV;SG;FUT
ʼoimed̥ ʼoyopo V;IPFV;PL;PRS
ʼoimed̥ ʼoime V;PRF;SG;PRS
ʼoimed̥ ʼoyopoad V;IPFV;PL;FUT
ʼoimed̥ ʼoime V;PRF;PL;PRS
ʼoimed̥ ʼoimed̥ V;IPFV;SG;PRS
ʼoimed̥ ʼoimed̥añ V;IMP;SG;PRS
ʼoimed̥ ʼoyopoiñ V;IMP;PL;PRS
sitolmad sitolmadad V;IPFV;PL;FUT
sitolmad sitolmadiñ V;IMP;SG;PRS
sitolmad sitolmad V;PRF;SG;PRS
sitolmad sitolmad V;IPFV;SG;PRS
sitolmad sitolmad V;IPFV;PL;PRS
sitolmad sitolmadad V;IPFV;SG;FUT
sitolmad sitolmad V;PRF;PL;PRS
sitolmad sitolmadiñ V;IMP;PL;PRS
ñeid ñeidiñ V;IMP;SG;PRS
ñeid ñeidad V;IPFV;SG;FUT
ñeid ñeid V;IPFV;SG;PRS
ñeid ñeidiñ V;IMP;PL;PRS
ñeid ñei V;PRF;SG;PRS
ñeid ñeidad V;IPFV;PL;FUT
ñeid ñei V;PRF;PL;PRS
ñeid ñeid V;IPFV;PL;PRS
dahă dahiwa V;PRF;SG;PRS
dahă dahiñ V;IMP;SG;PRS
dahă dahă V;IPFV;SG;PRS
dahă dad̥hă V;IPFV;PL;PRS
dahă dad̥had V;IPFV;PL;FUT
dahă dahad V;IPFV;SG;FUT
dahă dadhiwua V;PRF;PL;PRS
dahă dahiñ V;IMP;PL;PRS
wopopig wopopigiñ V;IMP;PL;PRS
wopopig wopopĭ V;PRF;PL;PRS
wopopig wopopig V;IPFV;PL;PRS
wopopig wopopigiñ V;IMP;SG;PRS
wopopig wopopĭ V;PRF;SG;PRS
wopopig wopopig V;IPFV;SG;PRS
wopopig wopopigad V;IPFV;SG;FUT
wopopig wopopigad V;IPFV;PL;FUT
dai dads̥ V;PRF;PL;PRS
dai dai V;PRF;SG;PRS
mansa:na mansa:na N;PL
mansa:na mansa:na N;SG
gogs gogogs N;PL
gogs gogs N;SG
s̥u:s̥k s̥u:s̥k N;PL
s̥u:s̥k s̥u:s̥k N;SG
towa towa N;SG
towa totwa N;PL
to:lo to:lo N;SG
to:lo totlo N;PL
nawoj nanwoj N;PL
nawoj nawoj N;SG
ʼiʼihog ʼiʼihog V;IPFV;SG;PRS
ʼiʼihog ʼiʼihogad V;IPFV;SG;FUT
ʼiʼihog ʼiʼihogiñ V;IMP;SG;PRS
ʼiʼihog ʼiʼihog V;IPFV;PL;PRS
ʼiʼihog ʼiʼiho V;PRF;SG;PRS
ʼiʼihog ʼiʼiho V;PRF;PL;PRS
ʼiʼihog ʼiʼihogad V;IPFV;PL;FUT
ʼiʼihog ʼiʼihogiñ V;IMP;PL;PRS
s-wihonig s-wihonigiñ V;IMP;SG;PRS
s-wihonig s-wiphionig V;IPFV;PL;PRS
s-wihonig s-wiphionigad V;IPFV;PL;FUT
s-wihonig s-wiphionigiñ V;IMP;PL;PRS
s-wihonig s-wihonigad V;IPFV;SG;FUT
s-wihonig s-wihonig V;IPFV;SG;PRS
ʼo:gĭ ʼoʼo:gĭ N;PL
ʼo:gĭ ʼo:gĭ N;SG
s̥onwuikud̥ s̥os̥onwuikud̥ N;PL
s̥onwuikud̥ s̥onwuikud̥ N;SG
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323a96affc5d49f67a95d961afd45dbb6c8fe2ef
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449d555969bfd7befe906877abab098c6e63a0e8
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/2300/CH5/EX5.7.9/Ex5_9.sce
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e95682590825c80b1d7f4a074190af0367044a16
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[] |
no_license
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
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Scilab
| false | false | 747 |
sce
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Ex5_9.sce
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//scilab 5.4.1
//windows 7 operating system
//chapter 5:Semiconductor Junction Diodes
clc
clear
V=15//V=supply voltage
Vz=12//Vz=Zener voltage
P=0.36//P=power of Zener diode
//P=Vz*I
I=(P/Vz)//I=maximum allowable Zener current
disp("A",I,"I=")
Iz=2*10^(-3)//Iz=minimum value attained by the zener current
Rl=1000//Rl=load resistance
i=Vz/Rl//i=load current
disp("A",i,"i=")
Imin=Iz+i//Imin=minimum allowable value of current
R=100//R=series resistance
Vr=Imin*R//Vr=voltage drop across R
disp("V",Vr,"Vr=")
Vmin=Vz+Vr//Vmin=minimum value of V
disp("V",Vmin,"Vmin=")
I1=I+i
disp("A",I1,"I1=")
VR=I1*R
disp("V",VR,"VR=")
Vmax=Vz+VR//Vmax=maximum value of V
disp("V",Vmax,"Vmax=")
disp("V can vary between Vmin & Vmax")
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7450ecfb0acbc0eeb9f447f3df1604dc5fb527e0
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449d555969bfd7befe906877abab098c6e63a0e8
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/380/CH6/EX6.7/Ex6_7.sce
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e6c8515060303c844711d67b1d768b0def0dee26
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[] |
no_license
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
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Scilab
| false | false | 464 |
sce
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Ex6_7.sce
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//Caption:Find the torque and efficiency of the motor
//Exa:6.7
clc;
clear;
close;
V_s=120;//in volts
N_m=2400;//speed of motor (in rpm)
I_in=7;//input current (in Amperes)
L=0.5;//arm length (in meter)
F_d=4.57;//deflection force (in Newton)
W=0.03;//weight (in Newton)
F=F_d-W;
T_s=F*L;
disp(T_s,'shaft torque of motor (in Newton-meter)=');
w_m=(2*%pi*N_m)/60;
P_o=T_s*w_m;
P_in=V_s*I_in;
Eff=P_o/P_in;
disp(Eff*100,'Efficiency of motor (%)=');
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3e68f4fe4c70ba8bd7ebe38d2bce41e4e4441017
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449d555969bfd7befe906877abab098c6e63a0e8
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/2873/CH10/EX10.9/Ex10_9.sce
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ae01a98e1befa76d7b2f87315ccb0edf76b010ea
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[] |
no_license
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
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Scilab
| false | false | 1,627 |
sce
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Ex10_9.sce
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// Display mode
mode(0);
// Display warning for floating point exception
ieee(1);
clear;
clc;
disp("Engineering Thermodynamics by Onkar Singh Chapter 10 Example 9")
h=10;//height of indicator diagram in mm
k=25;//indicator constant in KN/m^2 per mm
N=300;//engine rpm
Vs=1.5*10^-2;//swept volume in m^3
M=60;//effective brake load upon dynamometer in kg
r=50*10^-2;//effective brake drum radius in m
m=0.12;//fuel consumption in kg/min
C=42*10^3;//calorific value in KJ/kg
mw=6;//circulating water rate in kg/min
T1=35;//cooling water entering temperature in degree celcius
T2=70;//cooling water leaving temperature in degree celcius
Eg=30;//exhaust gases leaving energy in KJ/s
Cw=4.18;//specific heat of water in KJ/kg K
g=9.81;//accelaration due to gravity in m/s^2
disp("indicated mean effective pressure(P_imeb)=h*k in Kpa")
P_imeb=h*k
disp("indicated power(IP)=P_imeb*L*A*N/2 in KW")
IP=P_imeb*Vs*N/(2*60)
disp("brake power(BP)=2*%pi*N*T in KW")
BP=2*%pi*N*(M*g*r*10^-3)/(2*60)
disp("mechanical efficiency(n_mech)=BP/IP")
n_mech=BP/IP
disp("in percentage")
n_mech=n_mech*100
disp("so indicated power=9.375 KW")
disp("brake power=4.62 KW")
disp("mechanical efficiency=49.28%")
disp("energy liberated from fuel(Ef)=C*m/60 in KJ/s")
Ef=C*m/60
disp("energy available as brake power(BP)=4.62 KW")
disp("energy to coolant(Ec)=(mw/M)*Cw*(T2-T1) in KW")
Ec=(mw/M)*Cw*(T2-T1)
disp("energy carried by exhaust gases(Eg)=30 KJ/s")
disp("unaccounted energy loss=Ef-BP-Ec-Eg in KW")
Ef-BP-Ec-Eg
disp("NOTE=>overall energy balance sheet is attached as jpg file with this code.")
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449d555969bfd7befe906877abab098c6e63a0e8
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/323/CH6/EX6.7/ex6_7.sci
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f7679485dfd1beca7d4edb90ead40002e7761108
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[] |
no_license
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
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Scilab
| false | false | 286 |
sci
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ex6_7.sci
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//Ex6.7
clc;
V=100
Il=200
Rs=0.03
Rf=60
Ra=0.04
Vsfw=Il*Rs
printf("\n Voltage drop in series field winding =%.0f V \n",Vsfw)
If=(V+(Il*Rs))/Rf
printf("\n If=%.2f A \n",If)
Ia=Il+If
printf("\n Ia=%.2f A \n",Ia)
Eg=V+(Il*Rs)+(Ia*Ra)
printf("\n Generated EMF=%.2f V \n",Eg)
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61501742c489c99b61c9833c328726c3c31aba56
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449d555969bfd7befe906877abab098c6e63a0e8
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/1092/CH12/EX12.16/Example12_16.sce
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ad3581707924aaf79180d8a27a571fa6453b847e
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no_license
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
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Scilab
| false | false | 4,565 |
sce
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Example12_16.sce
|
// Electric Machinery and Transformers
// Irving L kosow
// Prentice Hall of India
// 2nd editiom
// Chapter 12: POWER,ENERGY,AND EFFICIENCY RELATIONS OF DC AND AC DYNAMOS
// Example 12-16
clear; clc; close; // Clear the work space and console.
// Given data
// code letter = J
P = 6 ; // Number of poles
S_r = 1176 ; // rotor speed in rpm
V = 220 ; // Rated voltage of SCIM in volt
f = 60 ; // Frequency in Hz
hp_SCIM = 7.5 ; // Power rating of SCIM in hp
R_ap = 0.3 ; // armature resistance in ohm/phase
R_r = 0.144 ; // rotor resistance in ohm/phase
jX_m = 13.5 ; // reactance in ohm/phase
jX_s = 0.5 ; // synchronous reactance in ohm/phase
jX_lr = 0.2 ; // Locked rotor reactance in ohm/phase
P_r = 300 ; // Rotational losses in W
disp("Example 12-16 : ");
// Calculations
S = (120*f/P); // Speed of synchronous magnetic field in rpm
// case a
s = (S-S_r)/S ; // Slip
R_r_by_s = R_r / s ;
// case b
printf(" \n From fig.12-11 , using the format method of mesh analysis,we may write");
printf(" \n the array by inspection :\n ");
printf(" \n_______________________________________________");
printf(" \n \t I_1 \t I_2 \t\t V ");
printf(" \n_______________________________________________");
printf(" \n\t (0.3+j14) -(0+j13.5) \t(127+j0)");
printf(" \n\t-(0+j13.5) (7.2+j13.7) \t 0");
printf(" \n_______________________________________________\n");
A = [ (0.3 + %i*14) -%i*13.5 ; (-%i*13.5) (7.2 + %i*13.7) ]; // Matrix containing above mesh eqns array
delta = det(A); // Determinant of A
// case b : Stator armature current I_p in A
I_p = det( [ (127+%i*0) (-%i*13.5) ; 0 (7.2 + %i*13.7) ] ) / delta ;
I_p_m = abs(I_p);//I_p_m=magnitude of I_p in A
I_p_a = atan(imag(I_p) /real(I_p))*180/%pi;//I_p_a=phase angle of I_p in degrees
I_1 = I_p ; // Stator armature current in A
// case c : Rotor current I_r per phase in A
I_r = det( [ (0.3 + %i*14) (127+%i*0) ; (-%i*13.5) 0 ] ) / delta ;
I_r_m = abs(I_r);//I_r_m=magnitude of I_r in A
I_r_a = atan(imag(I_r) /real(I_r))*180/%pi;//I_r_a=phase angle of I_r in degrees
// case d
theta = I_p_a ; // Motor PF angle in degrees
cos_theta = cosd(theta); // Motor PF
// case e
I_p = I_p_m ; // Stator armature current in A
V_p = V / sqrt(3); // Phase voltage in volt
SPI = V_p * I_p * cos_theta ; // Stator Power Input in W
// case f
SCL = (I_p)^2 * R_ap ; // Stator Copper Loss in W
// case g
// Subscripts 1 and 2 for RPI indicates two methods of calculating RPI
RPI_1 = SPI - SCL ; // Rotor Power Input in W
RPI_2 = (I_r_m)^2 * (R_r/s); // Rotor Power Input in W
RPI =RPI_1 ;
// case h
RCL = s*(RPI); // Rotor copper losses in W
// case i
// Subscripts 1 , 2 and 3 for RPD indicates three methods of calculating RPD
RPD_1 = RPI - RCL ; // Rotor Power Developed in W
RPD_2 = RPI * ( 1 - s ); // Rotor Power Developed in W
RPD = RPD_1 ;
// case j
RPO = 3*RPD - P_r ; // Rotor Power Developed in W
// case k
P_to = RPO ; // Total rotor power in W
T_o = (7.04*P_to)/S_r ; // Total 3-phase torque in lb-ft
// case l
hp = P_to / 746 ; // Output horsepower
// case m
P_in = 3*SPI ; // Input power to stator in W
P_o = RPO ; // Output power in W
eta = P_o / P_in * 100 ; // Motor efficiency at rated load
// Display the results
disp("Solution : ");
printf(" \n a: s = %.2f \n R_r/s = %.1f Ω \n",s,R_r_by_s );
printf(" \n Determinant Δ = ");disp(delta);
printf(" \n b: Stator armature current :\n I_p in A = ");disp(I_1);
printf(" \n I_p = I_1 = %.2f <%.2f A \n ",I_p_m , I_p_a );
printf(" \n c: Rotor current per phase :\n I_r in A = ");disp(I_r);
printf(" \n I_r = I_2 = %.3f <%.2f A \n ",I_r_m , I_r_a );
printf(" \n d: Motor PF :\n cosӨ = %.4f \n",cos_theta);
printf(" \n e: Stator Power Input :\n SPI = %d W \n",SPI);
printf(" \n f: Stator Copper Loss :\n SCL = %.1f W \n",SCL);
printf(" \n g: Rotor Power Input :\n RPI = %.1f W(method 1) ", RPI_1);
printf(" \n RPI = %.1f W (method 2)\n",RPI_2);
printf(" \n h: Rotor copper loss :\n RCL = %.1f W\n",RCL);
printf(" \n i: Rotor Power Developed :\n RPD = %.1f W \n",RPD_1);
printf(" \n RPD = %.1f W \n ",RPD_2);
printf(" \n j: Total 3-phase rotor power:\n RPO = %f W \n",RPO);
printf(" \n k: Total output torque developed :\n T_o = %.2f lb-ft\n",T_o);
printf(" \n l: Output horsepower : \n hp = %.2f hp (rated 7.5 hp)\n",hp);
printf(" \n m: Motor efficiency at rated load :\n η = %.2f percent \n",eta);
printf(" \n n: See Fig.12-12");
|
5835ef160926de3bbb159841f11aa76269443166
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1697/CH1/EX1.2/Exa1_2.sce
|
e91d77b3050c4107c57613f1eb6b54406529a87a
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 203 |
sce
|
Exa1_2.sce
|
//Exa 1.2
clc;
clear;
close;
//given data :
H=5.2;//in mA/m
Eta=120*%pi;//constant
//Formula : E/H=Eta
E=H*10^-3*Eta;//in V/m
disp(round(E),"Strength of Electric field in free space in V/m : ");
|
293b54479334c2643e38c8361009bcc42e856d2f
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2795/CH9/EX9.4/Ex9_04.sce
|
ae65e3792ce86e946cee80b95f994aa64b3320f3
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 835 |
sce
|
Ex9_04.sce
|
// Scilab Code Ex9.4: Page-310 (2014)
clc; clear;
m = 1; // For simplicity assume mass of gas molecule to be unity, kg
k = 1.38e-023; // Boltzmann constant, J/K
T = 293; // Room temperature, K
bita = k*T; // Energy associated with three degrees of freedom, J
v_mps = sqrt(2/(bita*m)); // For simplcity assume most probable speed to be unity, m/s
C = (bita*m/(2*%pi))^(3/2); // Constant in the distribution function
P = integrate('4*%pi*C*exp(-1/2*bita*m*v^2)*v^2', 'v', 0.99*v_mps, 1.01*v_mps);
printf("\nThe fraction of molecules in an ideal gas in equilibrium which have speeds within 1 percent above and below the most probable speed = %5.3f", P);
// Result
// The fraction of molecules in an ideal gas in equilibrium which have speeds within 1 percent above and below the most probable speed = 0.017
|
5ad51e5cf66b9c5a3a13d1ab3b01377d74eac7b2
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/43/CH6/EX6.3/ex6_3.sce
|
e0abf0ca7fe8763891827cf22813f8897571e08f
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 135 |
sce
|
ex6_3.sce
|
//Ex 6.3
clc;
syms s;
i=5;
R=2;
L=1;
C=1/2;
Z=((R+L*s)*(1/(C*s)))/((R+L*s)+(1/(C*s)));
V=Z*i;
v=ilaplace(V);
disp(v,'v(t)=');
|
6590dbd53070d6386805eacc8dad87af1a2e6dbf
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2579/CH5/EX5.5/Ex5_5.sce
|
fb8ff6a79432a6ea50172107d74df60eaeb5eed9
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 172 |
sce
|
Ex5_5.sce
|
//Ex:5.5
clc;
clear;
close;
Nm=1.24*10^6/10^6;// electron density in per m^3
fc=9*sqrt(Nm);// critical frequency in MHz
printf("The critical frequency = %f MHz", fc);
|
e6ea364f21c073865c5cd765cad381b08759b408
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2579/CH4/EX4.17/Ex4_17.sce
|
adf43af506c85736a6a7e20e607210be3c599b00
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 317 |
sce
|
Ex4_17.sce
|
//Ex:4.17
clc;
clear;
close;
r=0.45;// distance in m
f=10*10^3;// frequenc in MHz
y=300/f;// wavelength in m
Wtr=8.9;
wtr=10^(Wtr/10);
wrt=1/wtr;
D=(4*%pi*r/y)*(sqrt(wrt));// gain of the horn antenna
d=10*log(D)/log(10);// gain of the horn antenna in dB
printf("The gain of the horn antenna = %f dB", d);
|
1b7d587a6d0f9f446b0a7754767185c82f9df1e9
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/716/CH6/EX6.5.c/Solved_EX_6_5c.sce
|
b308b5c142c7922c24b41e1a8075fbd7eec6b747
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 444 |
sce
|
Solved_EX_6_5c.sce
|
//Determine even and odd parts of the signals x(n)={4,-4,2,-2}
clc;
clear;
x1={0 0 0 4 -4 2 -2};
plot2d3(x1);//for discrete plot
x2={-2 2 -4 4 0 0 0};
Xo=(x1/2-x2/2);
Xe=(x1/2+x2/2);
disp(Xo,'Odd part');
disp(Xe,'Even part');
xset('window',1);
subplot(1,2,1);
plot2d3(Xo);
xlabel("time");
ylabel("odd part");
subplot(1,2,2);
plot2d3(Xe);
xlabel("time");
ylabel("even part");
xset('window',2);
X=(Xo+Xe);
plot2d3(X);
|
a1000960af0d6609539a5795b07025befd0379f0
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2792/CH11/EX11.11/Ex11_11.sce
|
05b74da916a5e6682c785435cac44d206937859b
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,879 |
sce
|
Ex11_11.sce
|
clc
A= 10^-2
disp("A= "+string(A)+"cm^2") //initializing value of diode area
Na=5*10^16
disp("Na = "+string(Na)+"cm^-3") //initializing value of p side doping
Nd=5*10^17
disp("Nd = "+string(Nd)+"cm^-3") //initializing value of n side doping
Dn = 30
disp("Dn= "+string(Dn)+"cm^2/s")//initializing value of electron diffusion coefficient
Dp = 15
disp("Dp= "+string(Dp)+"cm^2/s")//initializing value of hole diffusion coefficient
Tn = 10^-8
disp("Tn= "+string(Tn)+"s")//inializing value of electron minority carrier lifetime
Tp = 10^-7
disp("Tp= "+string(Tp)+"s")//inializing value of hole minority carrier lifetime
e = 1.6*10^-19
disp("e= "+string(e)+"C")//initializing value of charge of electron
ni = 1.84*10^6
disp("ni = "+string(ni)+"cm^-3") //initializing value of intrinsic carrier concentration in GaAs
kbT = 0.026
disp("kbT = "+string(kbT)+"V/K") //initializing value of kbT at 300K
V = 1
disp("V = "+string(V)+"V") //initializing value of forward bias potential
nQr=.5
disp("nQr = "+string(nQr)) //initializing value of radiative recombination efficiency
Eph = 1.41
disp("Eph= "+string(Eph)+"eV")//initializing value of Energy of each photon
np = ni^2/Na
disp(" np = ni^2/Na= "+string(np)+"cm^-3")//calculation
pn = ni^2/Nd
disp(" pn = ni^2/Nd= "+string(pn)+"cm^-3")//calculation
Ln = sqrt(Dn*Tn)
disp("The electron diffusion length is ,Ln = sqrt(Dn*Tn)= "+string(Ln)+"cm")//calculation
Lp = sqrt(Dp*Tp)
disp("The hole diffusion length is ,Lp = sqrt(Dp*Tp)= "+string(Lp)+"cm")//calculation
In = ((A*e*Dn*np)/Ln)*(exp(V/kbT)-1)
disp("The injected current is ,In = ((A*e*Dn*np)/Ln)*(exp(V/kbT)-1)= "+string(In)+"A")//calculation
Iph = (In*nQr)/e
disp("The photon generated per second is ,Iph = (In*nQr)/e= "+string(Iph)+"s^-1")//calculation
P = Iph*e*Eph
disp("The optical power is ,P = Iph*e*Eph= "+string(P)+"W")//calculation
|
31aa01fb11803a17e9781dd81ab1825a676821a5
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2093/CH1/EX1.13/exa_1_13.sce
|
05990a6a50d83f2e3833bc9f55804187d13cb323
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 455 |
sce
|
exa_1_13.sce
|
// Exa 1.13
clc;
clear;
close;
// Given data
Rf= 250;// in kohm
// Output voltage expression, Vo= -5*Va+3*Vb
// and we know that for a difference amplifier circuit,
// Vo= -Rf/R1*Va + [R2/(R1+R2)]*[1+Rf/R1]*Vb
// Comparing both the expression, we get
// -Rf/R1*Va= -5*Va, or
R1= Rf/5;// in kohm
disp(R1,"The value of R1 in kohm")
// and
R2= 3*R1^2/(R1+Rf-3*R1)
disp(R2,"The value of R2 in kohm")
// Note : Answer in the book is wrong
|
1805f892e672b63e5443ee0c160900322f2ed6c1
|
717ddeb7e700373742c617a95e25a2376565112c
|
/2633/CH9/EX9.6/Ex9_6.sce
|
641dcaf30e2e505753bcdbcf18eedb5dc006c5a2
|
[] |
no_license
|
appucrossroads/Scilab-TBC-Uploads
|
b7ce9a8665d6253926fa8cc0989cda3c0db8e63d
|
1d1c6f68fe7afb15ea12fd38492ec171491f8ce7
|
refs/heads/master
| 2021-01-22T04:15:15.512674 | 2017-09-19T11:51:56 | 2017-09-19T11:51:56 | 92,444,732 | 0 | 0 | null | 2017-05-25T21:09:20 | 2017-05-25T21:09:19 | null |
UTF-8
|
Scilab
| false | false | 541 |
sce
|
Ex9_6.sce
|
clc
//initialisation of variables
d=30//in
w=50//lbf ft
d1=10//in
G=12*10^6//lbf/in^2
T1=50//lbf ft
T2=16.7//lbf ft
J=4810//lbf ft
TA=w/3//lbf ft
Tab=w-TA//lbf ft
//CALCULATIONS
Ta=Tab-TA//lbf ft
Qmax=T3*G*(3/8)/(%pi/32)*(3/4)^4//lbf/in^2
M=(T3*12*d1)/(%pi/4*(3/4)^4*G)*(180/%pi)//degree
//RESULTS
printf('The couples required to hold the ends=% f lbf ft',Ta)
printf('The magnitude of the greatest shear stress set up in the shaft=% f lbf/in^2',Qmax)
printf('the angular rotation in degree of the section=% f degree',M)
|
1698e35f616e98b621881923c6d97dfa610979a6
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/42/CH11/EX11.2/sadiku_11_2.sce
|
c4c50b0123e8b1218271115ca1c3c2c6110acad2
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 222 |
sce
|
sadiku_11_2.sce
|
clear;
clc;
Zo=60,a=20*10^-3,u=.6*3*10^8, f=100*10^6;
R=a*Zo,disp(R,'R=');
L=Zo/u,disp(L*10^9,'L in nH=');
G=a*a/R,disp(G*10^6,'G in micro S per meter =');
C=1/(u*Zo),disp(C*10^12,'C in pF =');
l=u/f;disp(l,'l=');
|
b5933887f9ded376957821eca3624c99b2e2914d
|
b9602336613b26d0b9c22a09d219c0ed8e158b4e
|
/Examples/Examples_VecFunc/cummulativeProduct.sce
|
84acbb06d553581766ec78636d327b981fbaf632
|
[
"BSD-2-Clause"
] |
permissive
|
CEG-MCA-Scilab-Hackathon/Scilab_Armadillo_Toolbox
|
d0a366f5f058ee45d3c4be7a41e08ed419d4b7cd
|
70c97cda4e0dd54df0a638e9b99f380c09ffa37e
|
refs/heads/master
| 2022-12-11T01:28:28.742041 | 2020-08-26T12:24:27 | 2020-08-26T12:24:27 | 290,481,428 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 206 |
sce
|
cummulativeProduct.sce
|
// Function Name: cummulativeProduct
// Calculate the cummulativeProduct for given array
// Calculating the cummulativeProduct.
inputvec1 = [1, 2, 3];
result = armaVec("cummulativeProduct",inputvec1)
|
325316d60adee4e47cfb01d4ee9dd9f8dbed4e37
|
a62e0da056102916ac0fe63d8475e3c4114f86b1
|
/set11/s_Fundamentals_Of_Engineering_Electromagnetics_S._Bhooshan_980.zip/Fundamentals_Of_Engineering_Electromagnetics_S._Bhooshan_980/CH1/EX1.3/1_3.sce
|
efae8b7d3f94dcb395d334a49130857d8a8e60cf
|
[] |
no_license
|
hohiroki/Scilab_TBC
|
cb11e171e47a6cf15dad6594726c14443b23d512
|
98e421ab71b2e8be0c70d67cca3ecb53eeef1df6
|
refs/heads/master
| 2021-01-18T02:07:29.200029 | 2016-04-29T07:01:39 | 2016-04-29T07:01:39 | null | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 275 |
sce
|
1_3.sce
|
errcatch(-1,"stop");mode(2);;
all;
format('v',11);
mod_a=sqrt(3^2+2^2);
mod_b=sqrt(15^2+3^2);
angle_a=atand(2/3);
angle_b=atand(3/15);
mod_ans=mod_a*mod_b;
angle_ans=angle_a+angle_b;
disp(angle_ans,"phase angle of ans(in degree)=",mod_ans,"mod of ans=");
exit();
|
f01fe51905d963e35d5659577491ff2152757f1d
|
a5de878687ee2e72db865481785dafbeda373e2a
|
/trunck/OpenPR-0.0.2/help/builder_help.sce
|
4d421c81c99694f5fe09580ede473f431f17292d
|
[
"BSD-3-Clause"
] |
permissive
|
Augertron/OpenPR
|
8f43102fd5811d26301ef75e0a1f2b6ba9cbdb73
|
e2b1ce89f020c1b25df8ac5d93f6a0014ed4f714
|
refs/heads/master
| 2020-05-15T09:31:08.385577 | 2011-03-21T02:51:40 | 2011-03-21T02:51:40 | 182,178,910 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 257 |
sce
|
builder_help.sce
|
help_dir = get_absolute_file_path('builder_help.sce');
tbx_builder_help_lang("en_US", help_dir);
helpdoc_path = help_dir+'en_US';
//xmltopdf(helpdoc_path, 'OpenPR Manual', 'en_US');
//xmltohtml(helpdoc_path, 'OpenPR Manual', 'en_US');
clear help_dir;
|
2e613272225e03fa0548108d40d38383bd156b26
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/647/CH2/EX2.4/Example2_4.sce
|
d72b423e01a3c37807e54a38b9410422bb70d2c9
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 662 |
sce
|
Example2_4.sce
|
clear;
clc;
// Example: 2.4
// Page: 41
printf("Example: 2.4 - Page: 41\n\n");
// Solution
//*****Data*****//
// From Fig. 2.4 (Page: 41)
// For process A-1-B:
Q1 = 60;// [kJ]
W1 = 35;// [kJ]
// For process A-2-B:
W2 = 50;// [kJ]
// For process B-3-A:
W3 = -70;// [kJ]
//************//
// For process A-1-B:
// The internal energy of the process A-1-B can be estimated as:
// Q = delta_U + W
delta_U = Q1 - W1;// [kJ]
// For process A-2-B:
Q2 = delta_U + W2;// [kJ]
// For process B-3-A:
Q3 = -delta_U + W3;// [kJ]
printf("The amount of heat transferred from the system to the surroundings during process B-3-A is %d kJ\n",-Q3);
|
74266ce2760dcd22fc2059314c8a68b4c09e5576
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/896/CH8/EX8.6/6.sce
|
85bd4184a26aedefba3204be11461a3d63bdca63
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,049 |
sce
|
6.sce
|
clc
//Example 8.6
//Calculate the cross sectional area, pressure, temperature and mach number at a pt in duct where air velocity is 1400ft/s
P1=30//psia
T1=660//R (Rankine temperature scale)
m=10//lbm/s mass flow rate
v1=1400//ft/s
R=4.98*10^4//(ft^2/s^2)*(lbm/lbmol.R)^0.5
k=1.4//dimentionless
M=29//lbm/lbmol
T2=T1-v1^2*((k-1)/k)*M/2/R//R (Rankine temperature scale)
printf("The temperature at the pt in the duct where air velocity is 1400 ft/s is %f R\n",T2);
c=223*(k*T2/M)^0.5//ft/s
Ma=v1/c//dimentionless (Mach number)
printf("The mach number at the pt in the duct where air velocity is 1400 ft/s is %f\n",Ma);
P2=P1/(T1/T2)^(k/(k-1))//psia
printf("The pressure at the pt in the duct where air velocity is 1400 ft/s is %f psia\n",P2);
//1 lbf.s^2 = 32.2 lbm.ft
A0=m/(P1*(M*k)^0.5*32.2/223/(T1)^0.5/((k-1)/2+1)^((k+1)/2/(k-1)))//in^2
ratio_A=((Ma^2*(k-1)/2+1)/((k-1)/2+1))^((k+1)/2/(k-1))/Ma//dimentionless
A=ratio_A*A0//in^2
printf("The cross sectional at the pt in the duct where air velocity is 1400 ft/s is %f in^2",A);
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4c741aa0b007ee35bfd173a228acd36e9fcb2a43
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3428/CH17/EX10.17.3/Ex10_17_3.sce
|
a72ab21968012216d6b3867fee0db6d6bd299c9f
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 279 |
sce
|
Ex10_17_3.sce
|
//Section-10,Example-2,Page no.-CT.29
//To find the largest mass which can be lifted through a height of 10 meters in the given expansion..
clc;
P_2=1
P_1=5
R=8.314
T=298
n=1
W=-(n*R*T)*log(P_1/P_2)
disp(W,'Maximum work done in(J)')
m_bar=-W/98.1
disp(m_bar,'Required mass(kg)')
|
2a58cb3e9c3e185afbcea1469d0a6893b950cee6
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1757/CH14/EX14.11/EX14_11.sce
|
a1bb07abfb4820991b60b44ac7126851704a10c4
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 2,121 |
sce
|
EX14_11.sce
|
// Example14.11 // Design a video amplifier of IC 1550 circuit
clc;
clear;
close;
Vcc = 12 ; // V
Av = -10 ;
Vagc = 0 ; // at bandwidth of 20 MHz
hfe = 50 ; // forward emitter parameter
rbb = 25 ; // ohm // base resistor
Cs = 1*10^-12 ; // F // source capacitor
Cl = 1*10^-12 ; // F // load capacitor
Ie1 = 1*10^-3 ; // A // emitter current of Q1
f = 1000*10^6 ; // Hz
Vt = 52*10^-3 ;
Vt1 = 0.026 ;
// When Vagc =0 the transistor Q2 is cut-off and the collector current of transistor Q2 flow through the transistor Q3
// i.e Ic1=Ie1=Ie3
Ie3 = 1*10^-3 ; // A // emitter current of Q3
Ic1 = 1*10^-3 ; // A // collector current of the transistor Q1
// it indicates that the emitter current of Q2 is zero Ie2 = 0 then the emitter resistor of Q2 is infinite
re2 = %inf ;
// emitter resistor of Q3
re3 = (Vt/Ie1);
disp('The emitter resistor of Q3 is = '+string(re3)+' ohm ');
// the trans conductance of transistor is
gm = (Ie1/Vt1);
disp('The trans conductance of transistor is = '+string(gm)+' A/V ');
// the base emitter resistor rbe
rbe = (hfe/gm);
disp('The base emitter resistor rbe is = '+string(rbe)+' ohm ');
// the emitter capacitor Ce
Ce = (gm/(2*%pi*f));
disp('The emitter capacitor is = '+string(Ce)+' F ');
// the voltage gain of video amplifier is
// Av = (Vo/Vin) ;
// Av = -((alpha3*gm)/(rbb*re3)*((1/rbb)+(1/rbe)+sCe)*((1/re2)+(1/re3)+sC3)*((1/Rl)+(s(Cs+Cl))))
// At Avgc = 0 i.e s=0 in the above Av equation
alpha3 = 1 ;
s = 0 ;
Av =-10 ;
Rl = -((alpha3*gm)/((rbb*re3)*(((1/rbb)+(1/rbe))*((1/re2)+(1/re3))*(Av))));
Rl = (1/Rl);
disp('The value of resistance RL is = '+string(Rl)+' ohm ');
// there are three poles present in the transfer function of video amplifier each pole generate one 3-db frequency
Rl = 265
fa = 1/(2*%pi*Rl*(Cs));
disp('The pole frequency fa is = '+string(fa)+' Hz ');
fb = 1/(2*%pi*Ce*((rbb*rbe)/(rbb+rbe)));
disp('The pole frequency fb is = '+string(fb)+' Hz ');
fc = 1/(2*%pi*Cs*re3);
disp('The pole frequency fc is = '+string(fc)+' Hz ');
disp(' Hence fa is a dominant pole frequency ');
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