/*************************************************************************** TITLE: engine.c ---------------------------------------------------------------------------- FUNCTION: dummy engine routine ---------------------------------------------------------------------------- MODULE STATUS: incomplete ---------------------------------------------------------------------------- GENEALOGY: This is a renamed navion_engine.c originall written by E. Bruce Jackson ---------------------------------------------------------------------------- DESIGNED BY: designer CODED BY: programmer MAINTAINED BY: maintainer ---------------------------------------------------------------------------- MODIFICATION HISTORY: DATE PURPOSE BY CURRENT RCS HEADER INFO: $Header$ * Revision 1.1 92/12/30 13:21:46 bjax * Initial revision * ---------------------------------------------------------------------------- REFERENCES: ---------------------------------------------------------------------------- CALLED BY: ls_model(); ---------------------------------------------------------------------------- CALLS TO: none ---------------------------------------------------------------------------- INPUTS: ---------------------------------------------------------------------------- OUTPUTS: --------------------------------------------------------------------------*/ #include #include "ls_types.h" #include "ls_constants.h" #include "ls_generic.h" #include "ls_sim_control.h" #include "ls_cockpit.h" #include "c172_aero.h" extern SIM_CONTROL sim_control_; void c172_engine( SCALAR dt, int init ) { float v,h,pa; float bhp=160; Throttle[3] = Throttle_pct; if ( ! Use_External_Engine ) { /* do a crude engine power calc based on throttle position */ v=V_rel_wind; h=Altitude; if(V_rel_wind < 10) v=10; if(Altitude < 0) h=0; pa=(0.00144*v + 0.546)*(1 - 1.6E-5*h)*bhp; if(pa < 0) pa=0; F_X_engine = Throttle[3]*(pa*550)/v; } else { /* accept external settings */ } /* printf("F_X_engine = %.3f\n", F_X_engine); */ M_m_engine = F_X_engine*0.734*cbar; /* 0.734 - estimated (WAGged) location of thrust line in the z-axis*/ }