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);
*/
}
+
+