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

More documents

Recommendations

Info

This channel also is etched into the motherboard. The Model II Cockpit, Book IV 11describes the electrical connections in detail with schematics and tables for each wiringconnection.2.5 Visual OutputThe visual output is split up into two sections, the front cockpit visuals and therear cockpit visuals. Each displays the pilot’s visuals and the Instructor Operating Station(IOS) visuals.2.5.1 Front Cockpit VisualsThe Spiegel computer also sends information about the aircraft to the visualcomputers. Figure 16 shows the front cockpitvisuals. The visuals are setup to generate threeviews. Eagle is designated as the center visualcomputer. Eagle will display the center view aswell as the HUD. Phantom and Pheagle willdisplay the left and right views respectively.Figure 16: Front Cockpit VisualsThe visuals can be either a Monterey database with an airport, or a Korean database withmountains.The pilot and the IOS have a set of visuals. Figure 17 shows the IOS visuals. TheIOS visuals are the same as the pilot’s visuals. This allows the operator to see where theaircraft is flying and still be able to monitor the state of the aircraft within the Simulinksimulation window. Also the operator can generate charts in real time or use any other20
tools that Simulink has to offer without stopping thesimulation. This allows data collection to be mucheasier and more robust. Operators can sendcommands to the pilot to get the data that they want.The IOS visuals also serve as a desktop simulator sooperators can fly and monitor the simulation bythemselves. This allows the operator to perform runFigure 17: Front Cockpit IOStime debugging without the help of others.2.5.1 Rear Cockpit VisualsThe rear cockpit simulation is similar to thefront cockpit, except that a single machine runs theback seat. The computer calculates the equations ofmotion, and displays the graphics. The rear cockpitis entirely separate from the front cockpit except forFigure 18: Rear Cockpit Visualsan Ethernet link. Figure 18 shows the back seat visual setup. A 15-inch flat screenmonitor is mounted in the back seat since a regular monitor would not fit.Similar to the front cockpit, the rear cockpithas an IOS. This serves the same purpose as the frontseat. Figure 19 Shows the IOS visuals for the rearcockpit. The increased visuals of all stations allowtwo pilots and two or more operators to monitor theaircraft’s states and the pilot’s maneuvers.Figure 19: Rear Cockpit IOS21
Page 1 and 2: Development of an Instrument Landin
Page 3 and 4: Approval PageTITLE: Development of
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 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
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/*****************
show all

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

Create successful ePaper yourself

Delete template?

Save as template?