else
elevator=(Long_control+long_trim)*23*DEG_TO_RAD;
- aileron = Lat_control*17.5*DEG_TO_RAD;
- rudder = Rudder_pedal*16*DEG_TO_RAD;
+ aileron = -1*Lat_control*17.5*DEG_TO_RAD;
+ rudder = -1*Rudder_pedal*16*DEG_TO_RAD;
/*
The aileron travel limits are 20 deg. TEU and 15 deg TED
but since we don't distinguish between left and right we'll
*//* printf("Maero: %7.4f Naero: %7.4f Raero: %7.4f\n",M_m_aero,M_n_aero,M_l_aero);
*/
}
+
+
/* F_X_engine = Throttle[3]*813.4/0.2; */ /* original code */
/* F_Z_engine = Throttle[3]*11.36/0.2; */ /* original code */
- F_X_engine = Throttle[3]*813.4/0.83;
- F_Z_engine = Throttle[3]*11.36/0.83;
+ F_X_engine = Throttle[3]*268.42/0.83;
+ F_Z_engine = Throttle[3]*3.75/0.83;
Throttle_pct = Throttle[3];
}
+
+
$Header$
$Log$
-Revision 1.4 1999/08/07 16:23:55 curt
+Revision 1.5 1999/08/07 17:18:45 curt
Updates to Tony's c172 model.
Revision 1.1.1.1 1999/04/05 21:32:45 curt
#include "ls_generic.h"
#include "ls_cockpit.h"
+/* SCALAR Brake_pct; */
void sub3( DATA v1[], DATA v2[], DATA result[] )
{
result[0] = v1[0] - v2[0];
}
-/* a quick navion_init.h */
-
-
-#ifndef _NAVION_INIT_H
-#define _NAVION_INIT_H
-
-
-void model_init( void );
-
-
-#endif _NAVION_INIT_H