I_yy = f.get_I_yy();
I_zz = f.get_I_zz();
I_xz = f.get_I_xz();
- Dx_pilot = f.get_Dx_pilot();
- Dy_pilot = f.get_Dy_pilot();
- Dz_pilot = f.get_Dz_pilot();
+ // Dx_pilot = f.get_Dx_pilot();
+ // Dy_pilot = f.get_Dy_pilot();
+ // Dz_pilot = f.get_Dz_pilot();
Dx_cg = f.get_Dx_cg();
Dy_cg = f.get_Dy_cg();
Dz_cg = f.get_Dz_cg();
- F_X = f.get_F_X();
- F_Y = f.get_F_Y();
- F_Z = f.get_F_Z();
- F_north = f.get_F_north();
- F_east = f.get_F_east();
- F_down = f.get_F_down();
- F_X_aero = f.get_F_X_aero();
- F_Y_aero = f.get_F_Y_aero();
- F_Z_aero = f.get_F_Z_aero();
- F_X_engine = f.get_F_X_engine();
- F_Y_engine = f.get_F_Y_engine();
- F_Z_engine = f.get_F_Z_engine();
- F_X_gear = f.get_F_X_gear();
- F_Y_gear = f.get_F_Y_gear();
- F_Z_gear = f.get_F_Z_gear();
- M_l_rp = f.get_M_l_rp();
- M_m_rp = f.get_M_m_rp();
- M_n_rp = f.get_M_n_rp();
- M_l_cg = f.get_M_l_cg();
- M_m_cg = f.get_M_m_cg();
- M_n_cg = f.get_M_n_cg();
- M_l_aero = f.get_M_l_aero();
- M_m_aero = f.get_M_m_aero();
- M_n_aero = f.get_M_n_aero();
- M_l_engine = f.get_M_l_engine();
- M_m_engine = f.get_M_m_engine();
- M_n_engine = f.get_M_n_engine();
- M_l_gear = f.get_M_l_gear();
- M_m_gear = f.get_M_m_gear();
- M_n_gear = f.get_M_n_gear();
- V_dot_north = f.get_V_dot_north();
- V_dot_east = f.get_V_dot_east();
- V_dot_down = f.get_V_dot_down();
- U_dot_body = f.get_U_dot_body();
- V_dot_body = f.get_V_dot_body();
- W_dot_body = f.get_W_dot_body();
- A_X_cg = f.get_A_X_cg();
- A_Y_cg = f.get_A_Y_cg();
- A_Z_cg = f.get_A_Z_cg();
- A_X_pilot = f.get_A_X_pilot();
- A_Y_pilot = f.get_A_Y_pilot();
- A_Z_pilot = f.get_A_Z_pilot();
- N_X_cg = f.get_N_X_cg();
- N_Y_cg = f.get_N_Y_cg();
- N_Z_cg = f.get_N_Z_cg();
- N_X_pilot = f.get_N_X_pilot();
- N_Y_pilot = f.get_N_Y_pilot();
- N_Z_pilot = f.get_N_Z_pilot();
- P_dot_body = f.get_P_dot_body();
- Q_dot_body = f.get_Q_dot_body();
- R_dot_body = f.get_R_dot_body();
+ // F_X = f.get_F_X();
+ // F_Y = f.get_F_Y();
+ // F_Z = f.get_F_Z();
+ // F_north = f.get_F_north();
+ // F_east = f.get_F_east();
+ // F_down = f.get_F_down();
+ // F_X_aero = f.get_F_X_aero();
+ // F_Y_aero = f.get_F_Y_aero();
+ // F_Z_aero = f.get_F_Z_aero();
+ // F_X_engine = f.get_F_X_engine();
+ // F_Y_engine = f.get_F_Y_engine();
+ // F_Z_engine = f.get_F_Z_engine();
+ // F_X_gear = f.get_F_X_gear();
+ // F_Y_gear = f.get_F_Y_gear();
+ // F_Z_gear = f.get_F_Z_gear();
+ // M_l_rp = f.get_M_l_rp();
+ // M_m_rp = f.get_M_m_rp();
+ // M_n_rp = f.get_M_n_rp();
+ // M_l_cg = f.get_M_l_cg();
+ // M_m_cg = f.get_M_m_cg();
+ // M_n_cg = f.get_M_n_cg();
+ // M_l_aero = f.get_M_l_aero();
+ // M_m_aero = f.get_M_m_aero();
+ // M_n_aero = f.get_M_n_aero();
+ // M_l_engine = f.get_M_l_engine();
+ // M_m_engine = f.get_M_m_engine();
+ // M_n_engine = f.get_M_n_engine();
+ // M_l_gear = f.get_M_l_gear();
+ // M_m_gear = f.get_M_m_gear();
+ // M_n_gear = f.get_M_n_gear();
+ // V_dot_north = f.get_V_dot_north();
+ // V_dot_east = f.get_V_dot_east();
+ // V_dot_down = f.get_V_dot_down();
+ // U_dot_body = f.get_U_dot_body();
+ // V_dot_body = f.get_V_dot_body();
+ // W_dot_body = f.get_W_dot_body();
+ // A_X_cg = f.get_A_X_cg();
+ // A_Y_cg = f.get_A_Y_cg();
+ // A_Z_cg = f.get_A_Z_cg();
+ // A_X_pilot = f.get_A_X_pilot();
+ // A_Y_pilot = f.get_A_Y_pilot();
+ // A_Z_pilot = f.get_A_Z_pilot();
+ // N_X_cg = f.get_N_X_cg();
+ // N_Y_cg = f.get_N_Y_cg();
+ // N_Z_cg = f.get_N_Z_cg();
+ // N_X_pilot = f.get_N_X_pilot();
+ // N_Y_pilot = f.get_N_Y_pilot();
+ // N_Z_pilot = f.get_N_Z_pilot();
+ // P_dot_body = f.get_P_dot_body();
+ // Q_dot_body = f.get_Q_dot_body();
+ // R_dot_body = f.get_R_dot_body();
V_north = f.get_V_north();
V_east = f.get_V_east();
V_down = f.get_V_down();
- V_north_rel_ground = f.get_V_north_rel_ground();
- V_east_rel_ground = f.get_V_east_rel_ground();
- V_down_rel_ground = f.get_V_down_rel_ground();
- V_north_airmass = f.get_V_north_airmass();
- V_east_airmass = f.get_V_east_airmass();
- V_down_airmass = f.get_V_down_airmass();
- V_north_rel_airmass = f.get_V_north_rel_airmass();
- V_east_rel_airmass = f.get_V_east_rel_airmass();
- V_down_rel_airmass = f.get_V_down_rel_airmass();
- U_gust = f.get_U_gust();
- V_gust = f.get_V_gust();
- W_gust = f.get_W_gust();
- U_body = f.get_U_body();
- V_body = f.get_V_body();
- W_body = f.get_W_body();
- V_rel_wind = f.get_V_rel_wind();
- V_true_kts = f.get_V_true_kts();
- V_rel_ground = f.get_V_rel_ground();
- V_inertial = f.get_V_inertial();
- V_ground_speed = f.get_V_ground_speed();
- V_equiv = f.get_V_equiv();
- V_equiv_kts = f.get_V_equiv_kts();
- V_calibrated = f.get_V_calibrated();
- V_calibrated_kts = f.get_V_calibrated_kts();
+ // V_north_rel_ground = f.get_V_north_rel_ground();
+ // V_east_rel_ground = f.get_V_east_rel_ground();
+ // V_down_rel_ground = f.get_V_down_rel_ground();
+ // V_north_airmass = f.get_V_north_airmass();
+ // V_east_airmass = f.get_V_east_airmass();
+ // V_down_airmass = f.get_V_down_airmass();
+ // V_north_rel_airmass = f.get_V_north_rel_airmass();
+ // V_east_rel_airmass = f.get_V_east_rel_airmass();
+ // V_down_rel_airmass = f.get_V_down_rel_airmass();
+ // U_gust = f.get_U_gust();
+ // V_gust = f.get_V_gust();
+ // W_gust = f.get_W_gust();
+ // U_body = f.get_U_body();
+ // V_body = f.get_V_body();
+ // W_body = f.get_W_body();
+ // V_rel_wind = f.get_V_rel_wind();
+ // V_true_kts = f.get_V_true_kts();
+ // V_rel_ground = f.get_V_rel_ground();
+ // V_inertial = f.get_V_inertial();
+ // V_ground_speed = f.get_V_ground_speed();
+ // V_equiv = f.get_V_equiv();
+ // V_equiv_kts = f.get_V_equiv_kts();
+ // V_calibrated = f.get_V_calibrated();
+ // V_calibrated_kts = f.get_V_calibrated_kts();
P_body = f.get_P_body();
Q_body = f.get_Q_body();
R_body = f.get_R_body();
- P_local = f.get_P_local();
- Q_local = f.get_Q_local();
- R_local = f.get_R_local();
- P_total = f.get_P_total();
- Q_total = f.get_Q_total();
- R_total = f.get_R_total();
- Phi_dot = f.get_Phi_dot();
- Theta_dot = f.get_Theta_dot();
- Psi_dot = f.get_Psi_dot();
- Latitude_dot = f.get_Latitude_dot();
- Longitude_dot = f.get_Longitude_dot();
- Radius_dot = f.get_Radius_dot();
+ // P_local = f.get_P_local();
+ // Q_local = f.get_Q_local();
+ // R_local = f.get_R_local();
+ // P_total = f.get_P_total();
+ // Q_total = f.get_Q_total();
+ // R_total = f.get_R_total();
+ // Phi_dot = f.get_Phi_dot();
+ // Theta_dot = f.get_Theta_dot();
+ // Psi_dot = f.get_Psi_dot();
+ // Latitude_dot = f.get_Latitude_dot();
+ // Longitude_dot = f.get_Longitude_dot();
+ // Radius_dot = f.get_Radius_dot();
Lat_geocentric = f.get_Lat_geocentric();
Lon_geocentric = f.get_Lon_geocentric();
Radius_to_vehicle = f.get_Radius_to_vehicle();
Phi = f.get_Phi();
Theta = f.get_Theta();
Psi = f.get_Psi();
- T_local_to_body_11 = f.get_T_local_to_body_11();
- T_local_to_body_12 = f.get_T_local_to_body_12();
- T_local_to_body_13 = f.get_T_local_to_body_13();
- T_local_to_body_21 = f.get_T_local_to_body_21();
- T_local_to_body_22 = f.get_T_local_to_body_22();
- T_local_to_body_23 = f.get_T_local_to_body_23();
- T_local_to_body_31 = f.get_T_local_to_body_31();
- T_local_to_body_32 = f.get_T_local_to_body_32();
- T_local_to_body_33 = f.get_T_local_to_body_33();
- Gravity = f.get_Gravity();
- Centrifugal_relief = f.get_Centrifugal_relief();
- Alpha = f.get_Alpha();
- Beta = f.get_Beta();
- Alpha_dot = f.get_Alpha_dot();
- Beta_dot = f.get_Beta_dot();
- Cos_alpha = f.get_Cos_alpha();
- Sin_alpha = f.get_Sin_alpha();
- Cos_beta = f.get_Cos_beta();
- Sin_beta = f.get_Sin_beta();
- Cos_phi = f.get_Cos_phi();
- Sin_phi = f.get_Sin_phi();
- Cos_theta = f.get_Cos_theta();
- Sin_theta = f.get_Sin_theta();
- Cos_psi = f.get_Cos_psi();
- Sin_psi = f.get_Sin_psi();
- Gamma_vert_rad = f.get_Gamma_vert_rad();
- Gamma_horiz_rad = f.get_Gamma_horiz_rad();
- Sigma = f.get_Sigma();
- Density = f.get_Density();
- V_sound = f.get_V_sound();
- Mach_number = f.get_Mach_number();
- Static_pressure = f.get_Static_pressure();
- Total_pressure = f.get_Total_pressure();
- Impact_pressure = f.get_Impact_pressure();
- Dynamic_pressure = f.get_Dynamic_pressure();
- Static_temperature = f.get_Static_temperature();
- Total_temperature = f.get_Total_temperature();
+ // T_local_to_body_11 = f.get_T_local_to_body_11();
+ // T_local_to_body_12 = f.get_T_local_to_body_12();
+ // T_local_to_body_13 = f.get_T_local_to_body_13();
+ // T_local_to_body_21 = f.get_T_local_to_body_21();
+ // T_local_to_body_22 = f.get_T_local_to_body_22();
+ // T_local_to_body_23 = f.get_T_local_to_body_23();
+ // T_local_to_body_31 = f.get_T_local_to_body_31();
+ // T_local_to_body_32 = f.get_T_local_to_body_32();
+ // T_local_to_body_33 = f.get_T_local_to_body_33();
+ // Gravity = f.get_Gravity();
+ // Centrifugal_relief = f.get_Centrifugal_relief();
+ // Alpha = f.get_Alpha();
+ // Beta = f.get_Beta();
+ // Alpha_dot = f.get_Alpha_dot();
+ // Beta_dot = f.get_Beta_dot();
+ // Cos_alpha = f.get_Cos_alpha();
+ // Sin_alpha = f.get_Sin_alpha();
+ // Cos_beta = f.get_Cos_beta();
+ // Sin_beta = f.get_Sin_beta();
+ // Cos_phi = f.get_Cos_phi();
+ // Sin_phi = f.get_Sin_phi();
+ // Cos_theta = f.get_Cos_theta();
+ // Sin_theta = f.get_Sin_theta();
+ // Cos_psi = f.get_Cos_psi();
+ // Sin_psi = f.get_Sin_psi();
+ // Gamma_vert_rad = f.get_Gamma_vert_rad();
+ // Gamma_horiz_rad = f.get_Gamma_horiz_rad();
+ // Sigma = f.get_Sigma();
+ // Density = f.get_Density();
+ // V_sound = f.get_V_sound();
+ // Mach_number = f.get_Mach_number();
+ // Static_pressure = f.get_Static_pressure();
+ // Total_pressure = f.get_Total_pressure();
+ // Impact_pressure = f.get_Impact_pressure();
+ // Dynamic_pressure = f.get_Dynamic_pressure();
+ // Static_temperature = f.get_Static_temperature();
+ // Total_temperature = f.get_Total_temperature();
Sea_level_radius = f.get_Sea_level_radius();
Earth_position_angle = f.get_Earth_position_angle();
Runway_altitude = f.get_Runway_altitude();
- Runway_latitude = f.get_Runway_latitude();
- Runway_longitude = f.get_Runway_longitude();
- Runway_heading = f.get_Runway_heading();
- Radius_to_rwy = f.get_Radius_to_rwy();
- D_cg_north_of_rwy = f.get_D_cg_north_of_rwy();
- D_cg_east_of_rwy = f.get_D_cg_east_of_rwy();
- D_cg_above_rwy = f.get_D_cg_above_rwy();
- X_cg_rwy = f.get_X_cg_rwy();
- Y_cg_rwy = f.get_Y_cg_rwy();
- H_cg_rwy = f.get_H_cg_rwy();
- D_pilot_north_of_rwy = f.get_D_pilot_north_of_rwy();
- D_pilot_east_of_rwy = f.get_D_pilot_east_of_rwy();
- D_pilot_above_rwy = f.get_D_pilot_above_rwy();
- X_pilot_rwy = f.get_X_pilot_rwy();
- Y_pilot_rwy = f.get_Y_pilot_rwy();
- H_pilot_rwy = f.get_H_pilot_rwy();
+ // Runway_latitude = f.get_Runway_latitude();
+ // Runway_longitude = f.get_Runway_longitude();
+ // Runway_heading = f.get_Runway_heading();
+ // Radius_to_rwy = f.get_Radius_to_rwy();
+ // D_cg_north_of_rwy = f.get_D_cg_north_of_rwy();
+ // D_cg_east_of_rwy = f.get_D_cg_east_of_rwy();
+ // D_cg_above_rwy = f.get_D_cg_above_rwy();
+ // X_cg_rwy = f.get_X_cg_rwy();
+ // Y_cg_rwy = f.get_Y_cg_rwy();
+ // H_cg_rwy = f.get_H_cg_rwy();
+ // D_pilot_north_of_rwy = f.get_D_pilot_north_of_rwy();
+ // D_pilot_east_of_rwy = f.get_D_pilot_east_of_rwy();
+ // D_pilot_above_rwy = f.get_D_pilot_above_rwy();
+ // X_pilot_rwy = f.get_X_pilot_rwy();
+ // Y_pilot_rwy = f.get_Y_pilot_rwy();
+ // H_pilot_rwy = f.get_H_pilot_rwy();
return( 0 );
}
// Convert from the LaRCsim generic_ struct to the FGState struct
int fgLaRCsim_2_FGState (FGState& 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_Pilot_Location( Dx_pilot, Dy_pilot, Dz_pilot );
f.set_CG_Position( Dx_cg, Dy_cg, Dz_cg );
// 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 );
+ // 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 );
+ // 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 );
+ // 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_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_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_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 );
+ // 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 );
+ 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_Gravity( Gravity );
+ // f.set_Centrifugal_relief( Centrifugal_relief );
- f.set_Alpha( Alpha );
+ // f.set_Alpha( Alpha );
f.set_Beta( Beta );
- f.set_Alpha_dot( Alpha_dot );
- f.set_Beta_dot( Beta_dot );
+ // 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_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_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_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_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_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_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_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 );
- 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 1.8 1998/12/18 23:37:06 curt
+// Collapsed out the FGState variables not currently needed. They are just
+// commented out and can be readded easily at any time. The point of this
+// exersize is to determine which variables were or were not currently being
+// used.
+//
// Revision 1.7 1998/12/14 13:31:06 curt
// LaRCsim maintains all it's variables internally. I had been copying all of
// them back and forth to the FG struture everytime I updated the flight model.
projects / flightgear.git / blobdiff