flapStruct flapper_struct;
//FlapStruct flapper_struct;
- flapper_alpha = Alpha*180/LS_PI;
+ flapper_alpha = Std_Alpha*180/LS_PI;
flapper_V = V_rel_wind;
flapper_freq = 0.8 + 0.45*Throttle_pct;
flapper_Inertia=flapper_struct.getInertia();
flapper_Moment=flapper_struct.getMoment();
- F_Z_aero_flapper = -1*flapper_Lift*cos(Alpha) - flapper_Thrust*sin(Alpha);
+ F_Z_aero_flapper = -1*flapper_Lift*cos(Std_Alpha) - flapper_Thrust*sin(Std_Alpha);
F_Z_aero_flapper -= flapper_Inertia;
- F_X_aero_flapper = -1*flapper_Lift*sin(Alpha) + flapper_Thrust*cos(Alpha);
+ F_X_aero_flapper = -1*flapper_Lift*sin(Std_Alpha) + flapper_Thrust*cos(Std_Alpha);
}