// Convert from the LaRCsim generic_ struct to the fgFLIGHT struct
int fgLaRCsim_2_Flight (fgFLIGHT& f) {
+ // Mass properties and geometry values
f.set_Inertias( Mass, I_xx, I_yy, I_zz, I_xz );
+ f.set_Pilot_Location( Dx_pilot, Dy_pilot, Dz_pilot );
+ f.set_CG_Position( Dx_cg, Dy_cg, Dz_cg );
- /*
- f.get_Dx_pilot() = Dx_pilot;
- f.get_Dy_pilot() = Dy_pilot;
- f.get_Dz_pilot() = Dz_pilot;
- f.get_Dx_cg() = Dx_cg;
- f.get_Dy_cg() = Dy_cg;
- f.get_Dz_cg() = Dz_cg;
- f.get_F_X() = F_X;
- f.get_F_Y() = F_Y;
- f.get_F_Z() = F_Z;
- f.get_F_north() = F_north;
- f.get_F_east() = F_east;
- f.get_F_down() = F_down;
- f.get_F_X_aero() = F_X_aero;
- f.get_F_Y_aero() = F_Y_aero;
- f.get_F_Z_aero() = F_Z_aero;
- f.get_F_X_engine() = F_X_engine;
- f.get_F_Y_engine() = F_Y_engine;
- f.get_F_Z_engine() = F_Z_engine;
- f.get_F_X_gear() = F_X_gear;
- f.get_F_Y_gear() = F_Y_gear;
- f.get_F_Z_gear() = F_Z_gear;
- f.get_M_l_rp() = M_l_rp;
- f.get_M_m_rp() = M_m_rp;
- f.get_M_n_rp() = M_n_rp;
- f.get_M_l_cg() = M_l_cg;
- f.get_M_m_cg() = M_m_cg;
- f.get_M_n_cg() = M_n_cg;
- f.get_M_l_aero() = M_l_aero;
- f.get_M_m_aero() = M_m_aero;
- f.get_M_n_aero() = M_n_aero;
- f.get_M_l_engine() = M_l_engine;
- f.get_M_m_engine() = M_m_engine;
- f.get_M_n_engine() = M_n_engine;
- f.get_M_l_gear() = M_l_gear;
- f.get_M_m_gear() = M_m_gear;
- f.get_M_n_gear() = M_n_gear;
- f.get_V_dot_north() = V_dot_north;
- f.get_V_dot_east() = V_dot_east;
- f.get_V_dot_down() = V_dot_down;
- f.get_U_dot_body() = U_dot_body;
- f.get_V_dot_body() = V_dot_body;
- f.get_W_dot_body() = W_dot_body;
- f.get_A_X_cg() = A_X_cg;
- f.get_A_Y_cg() = A_Y_cg;
- f.get_A_Z_cg() = A_Z_cg;
- f.get_A_X_pilot() = A_X_pilot;
- f.get_A_Y_pilot() = A_Y_pilot;
- f.get_A_Z_pilot() = A_Z_pilot;
- f.get_N_X_cg() = N_X_cg;
- f.get_N_Y_cg() = N_Y_cg;
- f.get_N_Z_cg() = N_Z_cg;
- f.get_N_X_pilot() = N_X_pilot;
- f.get_N_Y_pilot() = N_Y_pilot;
- f.get_N_Z_pilot() = N_Z_pilot;
- f.get_P_dot_body() = P_dot_body;
- f.get_Q_dot_body() = Q_dot_body;
- f.get_R_dot_body() = R_dot_body;
- f.get_V_north() = V_north;
- f.get_V_east() = V_east;
- f.get_V_down() = V_down;
- f.get_V_north_rel_ground() = V_north_rel_ground;
- f.get_V_east_rel_ground() = V_east_rel_ground;
- f.get_V_down_rel_ground() = V_down_rel_ground;
- f.get_V_north_airmass() = V_north_airmass;
- f.get_V_east_airmass() = V_east_airmass;
- f.get_V_down_airmass() = V_down_airmass;
- f.get_V_north_rel_airmass() = V_north_rel_airmass;
- f.get_V_east_rel_airmass() = V_east_rel_airmass;
- f.get_V_down_rel_airmass() = V_down_rel_airmass;
- f.get_U_gust() = U_gust;
- f.get_V_gust() = V_gust;
- f.get_W_gust() = W_gust;
- f.get_U_body() = U_body;
- f.get_V_body() = V_body;
- f.get_W_body() = W_body;
- f.get_V_rel_wind() = V_rel_wind;
- f.get_V_true_kts() = V_true_kts;
- f.get_V_rel_ground() = V_rel_ground;
- f.get_V_inertial() = V_inertial;
- f.get_V_ground_speed() = V_ground_speed;
- f.get_V_equiv() = V_equiv;
- f.get_V_equiv_kts() = V_equiv_kts;
- f.get_V_calibrated() = V_calibrated;
- f.get_V_calibrated_kts() = V_calibrated_kts;
- f.get_P_body() = P_body;
- f.get_Q_body() = Q_body;
- f.get_R_body() = R_body;
- f.get_P_local() = P_local;
- f.get_Q_local() = Q_local;
- f.get_R_local() = R_local;
- f.get_P_total() = P_total;
- f.get_Q_total() = Q_total;
- f.get_R_total() = R_total;
- f.get_Phi_dot() = Phi_dot;
- f.get_Theta_dot() = Theta_dot;
- f.get_Psi_dot() = Psi_dot;
- f.get_Latitude_dot() = Latitude_dot;
- f.get_Longitude_dot() = Longitude_dot;
- f.get_Radius_dot() = Radius_dot;
- f.get_Lat_geocentric() = Lat_geocentric;
- f.get_Lon_geocentric() = Lon_geocentric;
- f.get_Radius_to_vehicle() = Radius_to_vehicle;
- f.get_Latitude() = Latitude;
- f.get_Longitude() = Longitude;
- f.get_Altitude() = Altitude;
- f.get_Phi() = Phi;
- f.get_Theta() = Theta;
- f.get_Psi() = Psi;
- f.get_T_local_to_body_11() = T_local_to_body_11;
- f.get_T_local_to_body_12() = T_local_to_body_12;
- f.get_T_local_to_body_13() = T_local_to_body_13;
- f.get_T_local_to_body_21() = T_local_to_body_21;
- f.get_T_local_to_body_22() = T_local_to_body_22;
- f.get_T_local_to_body_23() = T_local_to_body_23;
- f.get_T_local_to_body_31() = T_local_to_body_31;
- f.get_T_local_to_body_32() = T_local_to_body_32;
- f.get_T_local_to_body_33() = T_local_to_body_33;
- f.get_Gravity() = Gravity;
- f.get_Centrifugal_relief() = Centrifugal_relief;
- f.get_Alpha() = Alpha;
- f.get_Beta() = Beta;
- f.get_Alpha_dot() = Alpha_dot;
- f.get_Beta_dot() = Beta_dot;
- f.get_Cos_alpha() = Cos_alpha;
- f.get_Sin_alpha() = Sin_alpha;
- f.get_Cos_beta() = Cos_beta;
- f.get_Sin_beta() = Sin_beta;
- f.get_Cos_phi() = Cos_phi;
- f.get_Sin_phi() = Sin_phi;
- f.get_Cos_theta() = Cos_theta;
- f.get_Sin_theta() = Sin_theta;
- f.get_Cos_psi() = Cos_psi;
- f.get_Sin_psi() = Sin_psi;
- f.get_Gamma_vert_rad() = Gamma_vert_rad;
- f.get_Gamma_horiz_rad() = Gamma_horiz_rad;
- f.get_Sigma() = Sigma;
- f.get_Density() = Density;
- f.get_V_sound() = V_sound;
- f.get_Mach_number() = Mach_number;
- f.get_Static_pressure() = Static_pressure;
- f.get_Total_pressure() = Total_pressure;
- f.get_Impact_pressure() = Impact_pressure;
- f.get_Dynamic_pressure() = Dynamic_pressure;
- f.get_Static_temperature() = Static_temperature;
- f.get_Total_temperature() = Total_temperature;
- f.get_Sea_level_radius() = Sea_level_radius;
- f.get_Earth_position_angle() = Earth_position_angle;
- f.get_Runway_altitude() = Runway_altitude;
- f.get_Runway_latitude() = Runway_latitude;
- f.get_Runway_longitude() = Runway_longitude;
- f.get_Runway_heading() = Runway_heading;
- f.get_Radius_to_rwy() = Radius_to_rwy;
- f.get_D_cg_north_of_rwy() = D_cg_north_of_rwy;
- f.get_D_cg_east_of_rwy() = D_cg_east_of_rwy;
- f.get_D_cg_above_rwy() = D_cg_above_rwy;
- f.get_X_cg_rwy() = X_cg_rwy;
- f.get_Y_cg_rwy() = Y_cg_rwy;
- f.get_H_cg_rwy() = H_cg_rwy;
- f.get_D_pilot_north_of_rwy() = D_pilot_north_of_rwy;
- f.get_D_pilot_east_of_rwy() = D_pilot_east_of_rwy;
- f.get_D_pilot_above_rwy() = D_pilot_above_rwy;
- f.get_X_pilot_rwy() = X_pilot_rwy;
- f.get_Y_pilot_rwy() = Y_pilot_rwy;
- f.get_H_pilot_rwy() = H_pilot_rwy;
- */
- return ( 0 );
+ // Forces
+ f.set_Forces_Body_Total( F_X, F_Y, F_Z );
+ f.set_Forces_Local_Total( F_north, F_east, F_down );
+ f.set_Forces_Aero( F_X_aero, F_Y_aero, F_Z_aero );
+ f.set_Forces_Engine( F_X_engine, F_Y_engine, F_Z_engine );
+ f.set_Forces_Gear( F_X_gear, F_Y_gear, F_Z_gear );
+
+ // Moments
+ f.set_Moments_Total_RP( M_l_rp, M_m_rp, M_n_rp );
+ f.set_Moments_Total_CG( M_l_cg, M_m_cg, M_n_cg );
+ f.set_Moments_Aero( M_l_aero, M_m_aero, M_n_aero );
+ f.set_Moments_Engine( M_l_engine, M_m_engine, M_n_engine );
+ f.set_Moments_Gear( M_l_gear, M_m_gear, M_n_gear );
+
+ // Accelerations
+ f.set_Accels_Local( V_dot_north, V_dot_east, V_dot_down );
+ f.set_Accels_Body( U_dot_body, V_dot_body, W_dot_body );
+ f.set_Accels_CG_Body( A_X_cg, A_Y_cg, A_Z_cg );
+ f.set_Accels_Pilot_Body( A_X_pilot, A_Y_pilot, A_Z_pilot );
+ f.set_Accels_CG_Body_N( N_X_cg, N_Y_cg, N_Z_cg );
+ f.set_Accels_Pilot_Body_N( N_X_pilot, N_Y_pilot, N_Z_pilot );
+ f.set_Accels_Omega( P_dot_body, Q_dot_body, R_dot_body );
+
+ // Velocities
+ f.set_Velocities_Local( V_north, V_east, V_down );
+ f.set_Velocities_Ground( V_north_rel_ground, V_east_rel_ground,
+ V_down_rel_ground );
+ f.set_Velocities_Local_Airmass( V_north_airmass, V_east_airmass,
+ V_down_airmass );
+ f.set_Velocities_Local_Rel_Airmass( V_north_rel_airmass, V_east_rel_airmass,
+ V_down_rel_airmass );
+ f.set_Velocities_Gust( U_gust, V_gust, W_gust );
+ f.set_Velocities_Wind_Body( U_body, V_body, W_body );
+
+ f.set_V_rel_wind( V_rel_wind );
+ f.set_V_true_kts( V_true_kts );
+ f.set_V_rel_ground( V_rel_ground );
+ f.set_V_inertial( V_inertial );
+ f.set_V_ground_speed( V_ground_speed );
+ f.set_V_equiv( V_equiv );
+ f.set_V_equiv_kts( V_equiv_kts );
+ f.set_V_calibrated( V_calibrated );
+ f.set_V_calibrated_kts( V_calibrated_kts );
+
+ f.set_Omega_Body( P_body, Q_body, R_body );
+ f.set_Omega_Local( P_local, Q_local, R_local );
+ f.set_Omega_Total( P_total, Q_total, R_total );
+
+ f.set_Euler_Rates( Phi_dot, Theta_dot, Psi_dot );
+ f.set_Geocentric_Rates( Latitude_dot, Longitude_dot, Radius_dot );
+
+ // Positions
+ f.set_Geocentric_Position( Lat_geocentric, Lon_geocentric,
+ Radius_to_vehicle );
+ f.set_Geodetic_Position( Latitude, Longitude, Altitude );
+ f.set_Euler_Angles( Phi, Theta, Psi );
+
+ // Miscellaneous quantities
+ f.set_T_Local_to_Body(T_local_to_body_m);
+ f.set_Gravity( Gravity );
+ f.set_Centrifugal_relief( Centrifugal_relief );
+
+ f.set_Alpha( Alpha );
+ f.set_Beta( Beta );
+ f.set_Alpha_dot( Alpha_dot );
+ f.set_Beta_dot( Beta_dot );
+
+ f.set_Cos_alpha( Cos_alpha );
+ f.set_Sin_alpha( Sin_alpha );
+ f.set_Cos_beta( Cos_beta );
+ f.set_Sin_beta( Sin_beta );
+
+ f.set_Cos_phi( Cos_phi );
+ f.set_Sin_phi( Sin_phi );
+ f.set_Cos_theta( Cos_theta );
+ f.set_Sin_theta( Sin_theta );
+ f.set_Cos_psi( Cos_psi );
+ f.set_Sin_psi( Sin_psi );
+
+ f.set_Gamma_vert_rad( Gamma_vert_rad );
+ f.set_Gamma_horiz_rad( Gamma_horiz_rad );
+
+ f.set_Sigma( Sigma );
+ f.set_Density( Density );
+ f.set_V_sound( V_sound );
+ f.set_Mach_number( Mach_number );
+
+ f.set_Static_pressure( Static_pressure );
+ f.set_Total_pressure( Total_pressure );
+ f.set_Impact_pressure( Impact_pressure );
+ f.set_Dynamic_pressure( Dynamic_pressure );
+
+ f.set_Static_temperature( Static_temperature );
+ f.set_Total_temperature( Total_temperature );
+
+ f.set_Sea_level_radius( Sea_level_radius );
+ f.set_Earth_position_angle( Earth_position_angle );
+
+ f.set_Runway_altitude( Runway_altitude );
+ f.set_Runway_latitude( Runway_latitude );
+ f.set_Runway_longitude( Runway_longitude );
+ f.set_Runway_heading( Runway_heading );
+ f.set_Radius_to_rwy( Radius_to_rwy );
+
+ f.set_CG_Rwy_Local( D_cg_north_of_rwy, D_cg_east_of_rwy, D_cg_above_rwy );
+ f.set_CG_Rwy_Rwy( X_cg_rwy, Y_cg_rwy, H_cg_rwy );
+ f.set_Pilot_Rwy_Local( D_pilot_north_of_rwy, D_pilot_east_of_rwy,
+ D_pilot_above_rwy );
+ f.set_Pilot_Rwy_Rwy( X_pilot_rwy, Y_pilot_rwy, H_pilot_rwy );
+
+ return 0;
}
// $Log$
+// Revision 1.5 1998/12/03 04:25:02 curt
+// Working on fixing up new fgFLIGHT class.
+//
// Revision 1.4 1998/12/03 01:16:37 curt
// Converted fgFLIGHT to a class.
//
projects / flightgear.git / blobdiff