Developement Of An Instrument Landing Simulation ... - Cal Poly

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* TSFCslAB=*uPtrs[8];* rho=*uPtrs[9];* a=*uPtrs[10];* Vtrue=*uPtrs[11];* Outputs:* y[0]=RFuelFlo;* y[1]=LFuelFlo;* y[2]=RThrust;* y[3]=LThrust;* y[4]=RNoz;* y[5]=LNoz;* y[6]=RRPM;* y[7]=LRPM;* y[8]=RTemp;* y[9]=LTemp;*/static void mdlOutputs(SimStruct *S, int_T tid){InputRealPtrsType uPtrs = ssGetInputPortRealSignalPtrs(S,0);real_T*y = ssGetOutputPortRealSignal(S,0);//Read in the Inputs:RFuelCap=*uPtrs[0];66
LFuelCap=*uPtrs[1];EngType=*uPtrs[2];Np=*uPtrs[3];RThrottle=*uPtrs[4];LThrottle=*uPtrs[5];Tsl=*uPtrs[6];TSFCslNAB=*uPtrs[7];TSFCslAB=*uPtrs[8];rho=*uPtrs[9];a=*uPtrs[10];Vtrue=*uPtrs[11];NumEng=*uPtrs[12];//<strong>Cal</strong>culate the Engine States:<strong>Cal</strong>culate();//Assign the Outputs:y[0]=RFuelFlo;y[1]=LFuelFlo;y[2]=RThrust;y[3]=LThrust;y[4]=RNoz;y[5]=LNoz;67
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Development of an Instrument Landin
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Approval PageTITLE: Development of
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AcknowledgementsI would like to tha
Page 8 and 9:
Figure 17: Front Cockpit IOS.......
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4.7.2 Throttle Calibration.........
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the simulation is transportable to
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development. These models had to be
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and right views respectively.Spiege
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The stick is connected to the stick
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Currently, the only console card in
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an output, it is sent from either t
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2.3 Computer SoftwareThe four compu
Page 26 and 27: 2.3.4 TCP-IP/UDPSince the computers
Page 28 and 29: 2.4 Analog OutputThe simulation sen
Page 30 and 31: This channel also is etched into th
Page 32 and 33: 3. Simulation Operations Procedures
Page 34 and 35: 3.2.1.2 Engine ModelThe engine mode
Page 36 and 37: 3.2.1.5 Instrument ModelThe instrum
Page 38 and 39: 3.2.2.1 Times Two TutorialThis is a
Page 40 and 41: 4.1.1 Terrain DatabaseFurther devel
Page 42 and 43: showing the pilot where he needs to
Page 44 and 45: 4.6 ProjectorsThe Visuals for the P
Page 46 and 47: Table 1: Instrument Calibration Che
Page 48 and 49: By adjusting the potentiometersetti
Page 50 and 51: 5. Simulator Implementation:The mos
Page 52 and 53: 5.4 Guidance and ControlsThe simula
Page 54 and 55: and visually see how an aircraft pe
Page 56 and 57: 14. Hill and Peterson, Mechanics an
Page 58 and 59: Documentation:Introduction to Pheag
Page 60 and 61: Stick ModelBelow is the Stick Model
Page 62 and 63: SixDOF ModelThis page describes the
Page 64 and 65: Standard Atmosphere ModelThis page
Page 66 and 67: Tutorial #1: Times Two TutorialThis
Page 68 and 69: Tutorial #2: Speed of Sound Tutoria
Page 70 and 71: B.1 Engine_Mod.c/* S-function engin
Page 72 and 73: * Also see Pheagle_HTML** Copyright
Page 74 and 75: ssSetInputPortWidth(S, 0, 13);//12
Page 78 and 79: y[6]=RRPM;y[7]=LRPM;y[8]=RTemp;y[9]
Page 80 and 81: High By-pass Engine: Engine Type =
Page 82 and 83: LThrust=LThrottle*Thrust;//printf("
Page 84 and 85: Calculate the Left Engine Nozzle Po
Page 86 and 87: B.2 Spool.c/***********************
Page 88 and 89: {ssSetNumSFcnParams(S, 0);if (ssGet
Page 90 and 91: * Initialize the state. Note, that
Page 92 and 93: * for performing any tasks that sho
Page 94 and 95: * S-function ils_modelB.3 ILS_Model
Page 96 and 97: #define S_FUNCTION_NAME ils_model//
Page 98 and 99: * Function: mdlInitializeSampleTime
Page 100 and 101: {InputRealPtrsType uPtrs = ssGetInp
Page 102 and 103: Theta2 = pi+Theta1;Theta3 = -((2*pi
Page 104 and 105: B.4 Server.c/**********************
Page 106 and 107: struct sockaddr_in you; // the outg
Page 108 and 109: #define MDL_START#if defined(MDL_ST
Page 110 and 111: {// This function sets the server s
Page 112 and 113: B.5 Server.h/**********************
Page 114 and 115: B.6 Slave.c/***********************
Page 116 and 117: ***********************************
Page 118 and 119: create the socketsocket_num=socket(
Page 120 and 121: host_data.ownrot.x = psi;host_data.
Page 122 and 123: B.7 ModHostData.h/*****************
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Developement Of An Instrument Landing Simulation ... - Cal Poly

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