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

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Authorization PageI grant permission for the republication of this thesis in its entity, or any of itsparts, without any further authorization by me.______________________Signature______________________Datei
Approval PageTITLE: Development of an Instrument Landing Simulationfor Cal Poly’s Flight Simulator using MATLAB/SimulinkAUTHOR: Robert A. BargerDATE: Friday, May 26 th , 2000__________________________________Dr. Daniel J. Biezad – Advisor__________________________________Signature__________________________________Dr. Jin Tso – Committee Member__________________________________Signature__________________________________Dr. Jordi Puig Suari – Committee Member__________________________________Signature__________________________________Edward Burnett – Committee Member__________________________________Signatureii
Page 1: Development of an Instrument Landin
Page 5: AcknowledgementsI would like to tha
Page 8 and 9: Figure 17: Front Cockpit IOS.......
Page 10 and 11: 4.7.2 Throttle Calibration.........
Page 12 and 13: the simulation is transportable to
Page 14 and 15: development. These models had to be
Page 16 and 17: and right views respectively.Spiege
Page 18 and 19: The stick is connected to the stick
Page 20 and 21: Currently, the only console card in
Page 22 and 23: an output, it is sent from either t
Page 24 and 25: 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 76 and 77:
* TSFCslAB=*uPtrs[8];* rho=*uPtrs[9
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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
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#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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