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

B.1 Engine_Mod.c/* S-function engine_mod* MODULE: engine_mod.c* AUTHOR(S): Robert A. Barger, Dieter Pestal, Dan Salluce* DATE: May 11, 2000* Copyright (c) ALL RIGHTS RESERVED** REVISION HISTORY:* REV AUTHOR DATE DESCRIPTION* 0 rab 5-11-00 Creation of code and Simulink Model** This C-file S-function simulates the engine model based on the current throttle*position as well as the current state that the engine is in. This engine model allows *fourdifferent types of engines to be modeled: (1) - Propeller piston engine, (2) - *Turboprop,(3) - Hi Bypass, (4) - Turbojet with Afterburner or without. The thrust* based on altitude, fuel flow, nozzle position, RPM, and engine temp are calculated.** Inputs:* RFuelCap* LFuelCap* EngType* Np - Prop Efficiency* RThrottle, %60