An Integrated, Modular Simulation System for Education ... - Cal Poly

More documents

Recommendations

Info

float K = 10.0;printf("\nEnter wn [natural frequency (rad./sec.)]\n");scanf("%f",&wn);// float wn = 0.12845;printf("\nEnter zeta (damping)\n");scanf("%f",&zeta);// float zeta = 0.724;float deltaE = 1.0;float dt = 0.5;float tFinal = 100;float a, b, c;float k1, l1, k2, l2, k3, l3, k4, l4;//***** end of inputs//***** coefficients <strong>for</strong> Runge-Kutta methoda = 2.0*zeta*wn;b = wn*wn;c = wn*wn;Theta[1]=0;z[1]=0;float t = dt;Time[1]=0;int index=2;while (t
{// write array to filefprintf(fout,"%lf ",Time[j]);if (feof (fout)) printf("End of file...\n");fprintf(fout,"\n");}fprintf(fout,"] theta=[ ");<strong>for</strong> (int l=1; l
Page 2:
Authorization PageI grant permissio
Page 6 and 7:
Table of ContentsLIST OF TABLESXIIL
Page 8 and 9:
Standard Atmosphere 64Input 65Outpu
Page 10 and 11:
RK4 (RUNGE-KUTTA) HELP FILE 91RK4 (
Page 12 and 13:
List of TablesTablePageTable 1. Air
Page 14 and 15:
Figure 27. Kaman SH2-F 72Figure 28.
Page 16 and 17:
has been developing a set of the ba
Page 18 and 19:
Simulink is a graphical user interf
Page 20 and 21:
computers are now fast enough to do
Page 22 and 23:
simulation after the conversion. Th
Page 24 and 25:
then a simple one axis closed loop
Page 26 and 27:
PhEagle IPhEagle Hardware - Sim Cab
Page 28 and 29:
highlight some text on a word proce
Page 30 and 31:
up to perform the less processor in
Page 32 and 33:
the Heads Up Display (HUD). While c
Page 34 and 35:
and monitors and computer code to s
Page 36 and 37:
Existing Simulation ToolsThere are
Page 38 and 39:
great control over the model dynami
Page 40 and 41:
Figure 11 BYOFS Original ScreenFigu
Page 42 and 43:
Basic 6-DOF Nonlinear, Rigid Body,
Page 44 and 45:
0 18 Cmu - Pitch moment due to forw
Page 46 and 47:
each of the linear force terms. The
Page 48 and 49:
PhEagle IIPhEagle II Introduction a
Page 50 and 51:
instructor a graphical interface to
Page 52 and 53:
Simulink block set, however, when m
Page 54 and 55:
existing graphics by creating a TCP
Page 56 and 57:
Simulink environment, and Mathworks
Page 58 and 59: D/A (output) block is the code for
Page 60 and 61: Table 9 Cab InputsInput from cab ou
Page 62 and 63: Key Features of SimulationsStabilit
Page 64 and 65: subsystem with inputs and outputs.
Page 66 and 67: viewer has the end of the runway co
Page 68 and 69: The 6 degree of freedom (3 translat
Page 70 and 71: difference between the two axes are
Page 72 and 73: Unit Delay1zelevatorelevElevElevato
Page 74 and 75: 6 DOF Model VerificationThe 6 DOF m
Page 76 and 77: oth models. The two state space mod
Page 78 and 79: Impulse ResponseRoll Angle32.5Ampli
Page 80 and 81: modeled. By feeding back any of the
Page 82 and 83: R10000 processors an inceptor Flybo
Page 84 and 85: directly to the Euler block the out
Page 86 and 87: function and the dynamics were very
Page 88 and 89: made by handling qualities engineer
Page 90 and 91: mode. The aircraft was divergent de
Page 92 and 93: simplified to resemble a spring-dam
Page 94 and 95: the data and converting to the prop
Page 96 and 97: ConclusionsConverting existing soft
Page 98 and 99: Future WorkPhEagle II provides basi
Page 100 and 101: workstation or PC for function test
Page 102 and 103: 13. Tischler, M. B.; Chen, R. T. N;
Page 104 and 105: AppendixEuler Help File%***** euler
Page 106 and 107: k4=dt*(z(index-1)+l3/2.0);l4=dt*(-a
Page 110 and 111: Snoopy 2nd order RK4 Class//-------
Page 112 and 113: {private:void CalcPowerDyn();void C
Page 114 and 115: int opMode;int oldVmode;int checkpt
Page 116 and 117: }exit_code = 0;}if (opMode != DEBUG
Page 118 and 119: }opMode = HELP;else if ((*argv[i] =
Page 120 and 121: Instrument D/A Simulink S-function/
Page 122 and 123: * Function: mdlInitializeSampleTime
Page 124 and 125: cdVerIndicator.channelNumber=5;cdVe
Page 126 and 127: set(&yawForceOut,*uPtrs[26]);set(&r
Page 128 and 129: Instrument Help Filefunctionallinst
Page 130 and 131: Stick D/A Simulink S-function/*****
Page 132 and 133: aToD12.cntCtrl=addr + 3;aToD12.da1L
Page 134 and 135: * with in an enabled subsystem whic
Page 136 and 137: #define MDL_DERIVATIVES /* Change t
Page 138 and 139: Abbreviated Instrument D/A Simulink
Page 140 and 141: {d16.nBits=16;d16.baseAddr=0x340;d1
Page 142 and 143: InputRealPtrsType uPtrs = ssGetInpu
Page 144 and 145: #ifdef MATLAB_MEX_FILE /* Is this f
Page 146 and 147: Abbreviated Stick D/A Simulink S-fu
Page 148 and 149: aToD12.da2Low=addr + 6;aToD12.da2Hi
Page 150 and 151: */static void mdlDerivatives(SimStr
Page 152 and 153: Header file for Stick S-functions//
Page 154 and 155: Abbreviated Stick Help filefunction
Page 156 and 157: #define Deg2Rad 0.01745329#define R
Page 158 and 159:
* Parameter Value Description* Name
Page 160 and 161:
* y[15]= qDot* y[16]= rDot* y[17]=
Page 162 and 163:
***** Compute the rolling moment ex
Page 164 and 165:
xDot=u*CTheta*CPsi+v*(SPhi*STheta*C
Page 166 and 167:
SAD file: Navion.tsf2.153 1 Alt1 [f
Page 168 and 169:
% | sAcB -sAsB cA | Fzb% Test dataF
Page 170 and 171:
Standard Atmosphere Simulink S-func
Page 172 and 173:
* in estimate();** Alt=*uPtrs[0]; m
Page 174 and 175:
Euler Coordinate Transform and Inte
Page 176 and 177:
* Abstract:* Specifiy that we inher
Page 178 and 179:
* calulate the trig functions first
Page 180 and 181:
Euler Transform Help Filefunction [
Page 182 and 183:
Game Joystick Driver Simulink S-fun
Page 184 and 185:
*/static void mdlInitializeConditio
Page 186 and 187:
* This function is called once for
Page 188 and 189:
Navion Longitudianal State Space Se
Page 190 and 191:
ANavionLatB=[0 .07045610 028.73202
Page 192 and 193:
Navion Longitudinal State Space Set
Page 194 and 195:
NNavionLatB=[0 0.070456128.73202 2.
Page 196:
% create a frequency vectorw=0.1:0.
show all

An Integrated, Modular Simulation System for Education ... - Cal Poly

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?