From ef4d103735dd1c63338e0c095a65976d0088cbbd Mon Sep 17 00:00:00 2001 From: curt Date: Mon, 14 Dec 1998 13:27:47 +0000 Subject: [PATCH] Removed some old, outdated, no longer needed code. --- LaRCsim/ls_interface.c | 356 +---------------------------------------- 1 file changed, 3 insertions(+), 353 deletions(-) diff --git a/LaRCsim/ls_interface.c b/LaRCsim/ls_interface.c index 0a12df1dd..dc311d87f 100644 --- a/LaRCsim/ls_interface.c +++ b/LaRCsim/ls_interface.c @@ -563,359 +563,6 @@ int ls_update(int multiloop) { } -#if 0 -/* Convert from the fgFLIGHT struct to the LaRCsim generic_ struct */ -int fgFlight_2_LaRCsim (fgFLIGHT *f) { - Mass = FG_Mass; - I_xx = FG_I_xx; - I_yy = FG_I_yy; - I_zz = FG_I_zz; - I_xz = FG_I_xz; - Dx_pilot = FG_Dx_pilot; - Dy_pilot = FG_Dy_pilot; - Dz_pilot = FG_Dz_pilot; - Dx_cg = FG_Dx_cg; - Dy_cg = FG_Dy_cg; - Dz_cg = FG_Dz_cg; - F_X = FG_F_X; - F_Y = FG_F_Y; - F_Z = FG_F_Z; - F_north = FG_F_north; - F_east = FG_F_east; - F_down = FG_F_down; - F_X_aero = FG_F_X_aero; - F_Y_aero = FG_F_Y_aero; - F_Z_aero = FG_F_Z_aero; - F_X_engine = FG_F_X_engine; - F_Y_engine = FG_F_Y_engine; - F_Z_engine = FG_F_Z_engine; - F_X_gear = FG_F_X_gear; - F_Y_gear = FG_F_Y_gear; - F_Z_gear = FG_F_Z_gear; - M_l_rp = FG_M_l_rp; - M_m_rp = FG_M_m_rp; - M_n_rp = FG_M_n_rp; - M_l_cg = FG_M_l_cg; - M_m_cg = FG_M_m_cg; - M_n_cg = FG_M_n_cg; - M_l_aero = FG_M_l_aero; - M_m_aero = FG_M_m_aero; - M_n_aero = FG_M_n_aero; - M_l_engine = FG_M_l_engine; - M_m_engine = FG_M_m_engine; - M_n_engine = FG_M_n_engine; - M_l_gear = FG_M_l_gear; - M_m_gear = FG_M_m_gear; - M_n_gear = FG_M_n_gear; - V_dot_north = FG_V_dot_north; - V_dot_east = FG_V_dot_east; - V_dot_down = FG_V_dot_down; - U_dot_body = FG_U_dot_body; - V_dot_body = FG_V_dot_body; - W_dot_body = FG_W_dot_body; - A_X_cg = FG_A_X_cg; - A_Y_cg = FG_A_Y_cg; - A_Z_cg = FG_A_Z_cg; - A_X_pilot = FG_A_X_pilot; - A_Y_pilot = FG_A_Y_pilot; - A_Z_pilot = FG_A_Z_pilot; - N_X_cg = FG_N_X_cg; - N_Y_cg = FG_N_Y_cg; - N_Z_cg = FG_N_Z_cg; - N_X_pilot = FG_N_X_pilot; - N_Y_pilot = FG_N_Y_pilot; - N_Z_pilot = FG_N_Z_pilot; - P_dot_body = FG_P_dot_body; - Q_dot_body = FG_Q_dot_body; - R_dot_body = FG_R_dot_body; - V_north = FG_V_north; - V_east = FG_V_east; - V_down = FG_V_down; - V_north_rel_ground = FG_V_north_rel_ground; - V_east_rel_ground = FG_V_east_rel_ground; - V_down_rel_ground = FG_V_down_rel_ground; - V_north_airmass = FG_V_north_airmass; - V_east_airmass = FG_V_east_airmass; - V_down_airmass = FG_V_down_airmass; - V_north_rel_airmass = FG_V_north_rel_airmass; - V_east_rel_airmass = FG_V_east_rel_airmass; - V_down_rel_airmass = FG_V_down_rel_airmass; - U_gust = FG_U_gust; - V_gust = FG_V_gust; - W_gust = FG_W_gust; - U_body = FG_U_body; - V_body = FG_V_body; - W_body = FG_W_body; - V_rel_wind = FG_V_rel_wind; - V_true_kts = FG_V_true_kts; - V_rel_ground = FG_V_rel_ground; - V_inertial = FG_V_inertial; - V_ground_speed = FG_V_ground_speed; - V_equiv = FG_V_equiv; - V_equiv_kts = FG_V_equiv_kts; - V_calibrated = FG_V_calibrated; - V_calibrated_kts = FG_V_calibrated_kts; - P_body = FG_P_body; - Q_body = FG_Q_body; - R_body = FG_R_body; - P_local = FG_P_local; - Q_local = FG_Q_local; - R_local = FG_R_local; - P_total = FG_P_total; - Q_total = FG_Q_total; - R_total = FG_R_total; - Phi_dot = FG_Phi_dot; - Theta_dot = FG_Theta_dot; - Psi_dot = FG_Psi_dot; - Latitude_dot = FG_Latitude_dot; - Longitude_dot = FG_Longitude_dot; - Radius_dot = FG_Radius_dot; - Lat_geocentric = FG_Lat_geocentric; - Lon_geocentric = FG_Lon_geocentric; - Radius_to_vehicle = FG_Radius_to_vehicle; - Latitude = FG_Latitude; - Longitude = FG_Longitude; - Altitude = FG_Altitude; - Phi = FG_Phi; - Theta = FG_Theta; - Psi = FG_Psi; - T_local_to_body_11 = FG_T_local_to_body_11; - T_local_to_body_12 = FG_T_local_to_body_12; - T_local_to_body_13 = FG_T_local_to_body_13; - T_local_to_body_21 = FG_T_local_to_body_21; - T_local_to_body_22 = FG_T_local_to_body_22; - T_local_to_body_23 = FG_T_local_to_body_23; - T_local_to_body_31 = FG_T_local_to_body_31; - T_local_to_body_32 = FG_T_local_to_body_32; - T_local_to_body_33 = FG_T_local_to_body_33; - Gravity = FG_Gravity; - Centrifugal_relief = FG_Centrifugal_relief; - Alpha = FG_Alpha; - Beta = FG_Beta; - Alpha_dot = FG_Alpha_dot; - Beta_dot = FG_Beta_dot; - Cos_alpha = FG_Cos_alpha; - Sin_alpha = FG_Sin_alpha; - Cos_beta = FG_Cos_beta; - Sin_beta = FG_Sin_beta; - Cos_phi = FG_Cos_phi; - Sin_phi = FG_Sin_phi; - Cos_theta = FG_Cos_theta; - Sin_theta = FG_Sin_theta; - Cos_psi = FG_Cos_psi; - Sin_psi = FG_Sin_psi; - Gamma_vert_rad = FG_Gamma_vert_rad; - Gamma_horiz_rad = FG_Gamma_horiz_rad; - Sigma = FG_Sigma; - Density = FG_Density; - V_sound = FG_V_sound; - Mach_number = FG_Mach_number; - Static_pressure = FG_Static_pressure; - Total_pressure = FG_Total_pressure; - Impact_pressure = FG_Impact_pressure; - Dynamic_pressure = FG_Dynamic_pressure; - Static_temperature = FG_Static_temperature; - Total_temperature = FG_Total_temperature; - Sea_level_radius = FG_Sea_level_radius; - Earth_position_angle = FG_Earth_position_angle; - Runway_altitude = FG_Runway_altitude; - Runway_latitude = FG_Runway_latitude; - Runway_longitude = FG_Runway_longitude; - Runway_heading = FG_Runway_heading; - Radius_to_rwy = FG_Radius_to_rwy; - D_cg_north_of_rwy = FG_D_cg_north_of_rwy; - D_cg_east_of_rwy = FG_D_cg_east_of_rwy; - D_cg_above_rwy = FG_D_cg_above_rwy; - X_cg_rwy = FG_X_cg_rwy; - Y_cg_rwy = FG_Y_cg_rwy; - H_cg_rwy = FG_H_cg_rwy; - D_pilot_north_of_rwy = FG_D_pilot_north_of_rwy; - D_pilot_east_of_rwy = FG_D_pilot_east_of_rwy; - D_pilot_above_rwy = FG_D_pilot_above_rwy; - X_pilot_rwy = FG_X_pilot_rwy; - Y_pilot_rwy = FG_Y_pilot_rwy; - H_pilot_rwy = FG_H_pilot_rwy; - - return( 0 ); -} - - -/* Convert from the LaRCsim generic_ struct to the fgFLIGHT struct */ -int fgLaRCsim_2_Flight (fgFLIGHT *f) { - FG_Mass = Mass; - FG_I_xx = I_xx; - FG_I_yy = I_yy; - FG_I_zz = I_zz; - FG_I_xz = I_xz; - FG_Dx_pilot = Dx_pilot; - FG_Dy_pilot = Dy_pilot; - FG_Dz_pilot = Dz_pilot; - FG_Dx_cg = Dx_cg; - FG_Dy_cg = Dy_cg; - FG_Dz_cg = Dz_cg; - FG_F_X = F_X; - FG_F_Y = F_Y; - FG_F_Z = F_Z; - FG_F_north = F_north; - FG_F_east = F_east; - FG_F_down = F_down; - FG_F_X_aero = F_X_aero; - FG_F_Y_aero = F_Y_aero; - FG_F_Z_aero = F_Z_aero; - FG_F_X_engine = F_X_engine; - FG_F_Y_engine = F_Y_engine; - FG_F_Z_engine = F_Z_engine; - FG_F_X_gear = F_X_gear; - FG_F_Y_gear = F_Y_gear; - FG_F_Z_gear = F_Z_gear; - FG_M_l_rp = M_l_rp; - FG_M_m_rp = M_m_rp; - FG_M_n_rp = M_n_rp; - FG_M_l_cg = M_l_cg; - FG_M_m_cg = M_m_cg; - FG_M_n_cg = M_n_cg; - FG_M_l_aero = M_l_aero; - FG_M_m_aero = M_m_aero; - FG_M_n_aero = M_n_aero; - FG_M_l_engine = M_l_engine; - FG_M_m_engine = M_m_engine; - FG_M_n_engine = M_n_engine; - FG_M_l_gear = M_l_gear; - FG_M_m_gear = M_m_gear; - FG_M_n_gear = M_n_gear; - FG_V_dot_north = V_dot_north; - FG_V_dot_east = V_dot_east; - FG_V_dot_down = V_dot_down; - FG_U_dot_body = U_dot_body; - FG_V_dot_body = V_dot_body; - FG_W_dot_body = W_dot_body; - FG_A_X_cg = A_X_cg; - FG_A_Y_cg = A_Y_cg; - FG_A_Z_cg = A_Z_cg; - FG_A_X_pilot = A_X_pilot; - FG_A_Y_pilot = A_Y_pilot; - FG_A_Z_pilot = A_Z_pilot; - FG_N_X_cg = N_X_cg; - FG_N_Y_cg = N_Y_cg; - FG_N_Z_cg = N_Z_cg; - FG_N_X_pilot = N_X_pilot; - FG_N_Y_pilot = N_Y_pilot; - FG_N_Z_pilot = N_Z_pilot; - FG_P_dot_body = P_dot_body; - FG_Q_dot_body = Q_dot_body; - FG_R_dot_body = R_dot_body; - FG_V_north = V_north; - FG_V_east = V_east; - FG_V_down = V_down; - FG_V_north_rel_ground = V_north_rel_ground; - FG_V_east_rel_ground = V_east_rel_ground; - FG_V_down_rel_ground = V_down_rel_ground; - FG_V_north_airmass = V_north_airmass; - FG_V_east_airmass = V_east_airmass; - FG_V_down_airmass = V_down_airmass; - FG_V_north_rel_airmass = V_north_rel_airmass; - FG_V_east_rel_airmass = V_east_rel_airmass; - FG_V_down_rel_airmass = V_down_rel_airmass; - FG_U_gust = U_gust; - FG_V_gust = V_gust; - FG_W_gust = W_gust; - FG_U_body = U_body; - FG_V_body = V_body; - FG_W_body = W_body; - FG_V_rel_wind = V_rel_wind; - FG_V_true_kts = V_true_kts; - FG_V_rel_ground = V_rel_ground; - FG_V_inertial = V_inertial; - FG_V_ground_speed = V_ground_speed; - FG_V_equiv = V_equiv; - FG_V_equiv_kts = V_equiv_kts; - FG_V_calibrated = V_calibrated; - FG_V_calibrated_kts = V_calibrated_kts; - FG_P_body = P_body; - FG_Q_body = Q_body; - FG_R_body = R_body; - FG_P_local = P_local; - FG_Q_local = Q_local; - FG_R_local = R_local; - FG_P_total = P_total; - FG_Q_total = Q_total; - FG_R_total = R_total; - FG_Phi_dot = Phi_dot; - FG_Theta_dot = Theta_dot; - FG_Psi_dot = Psi_dot; - FG_Latitude_dot = Latitude_dot; - FG_Longitude_dot = Longitude_dot; - FG_Radius_dot = Radius_dot; - FG_Lat_geocentric = Lat_geocentric; - FG_Lon_geocentric = Lon_geocentric; - FG_Radius_to_vehicle = Radius_to_vehicle; - FG_Latitude = Latitude; - FG_Longitude = Longitude; - FG_Altitude = Altitude; - FG_Phi = Phi; - FG_Theta = Theta; - FG_Psi = Psi; - FG_T_local_to_body_11 = T_local_to_body_11; - FG_T_local_to_body_12 = T_local_to_body_12; - FG_T_local_to_body_13 = T_local_to_body_13; - FG_T_local_to_body_21 = T_local_to_body_21; - FG_T_local_to_body_22 = T_local_to_body_22; - FG_T_local_to_body_23 = T_local_to_body_23; - FG_T_local_to_body_31 = T_local_to_body_31; - FG_T_local_to_body_32 = T_local_to_body_32; - FG_T_local_to_body_33 = T_local_to_body_33; - FG_Gravity = Gravity; - FG_Centrifugal_relief = Centrifugal_relief; - FG_Alpha = Alpha; - FG_Beta = Beta; - FG_Alpha_dot = Alpha_dot; - FG_Beta_dot = Beta_dot; - FG_Cos_alpha = Cos_alpha; - FG_Sin_alpha = Sin_alpha; - FG_Cos_beta = Cos_beta; - FG_Sin_beta = Sin_beta; - FG_Cos_phi = Cos_phi; - FG_Sin_phi = Sin_phi; - FG_Cos_theta = Cos_theta; - FG_Sin_theta = Sin_theta; - FG_Cos_psi = Cos_psi; - FG_Sin_psi = Sin_psi; - FG_Gamma_vert_rad = Gamma_vert_rad; - FG_Gamma_horiz_rad = Gamma_horiz_rad; - FG_Sigma = Sigma; - FG_Density = Density; - FG_V_sound = V_sound; - FG_Mach_number = Mach_number; - FG_Static_pressure = Static_pressure; - FG_Total_pressure = Total_pressure; - FG_Impact_pressure = Impact_pressure; - FG_Dynamic_pressure = Dynamic_pressure; - FG_Static_temperature = Static_temperature; - FG_Total_temperature = Total_temperature; - FG_Sea_level_radius = Sea_level_radius; - FG_Earth_position_angle = Earth_position_angle; - FG_Runway_altitude = Runway_altitude; - FG_Runway_latitude = Runway_latitude; - FG_Runway_longitude = Runway_longitude; - FG_Runway_heading = Runway_heading; - FG_Radius_to_rwy = Radius_to_rwy; - FG_D_cg_north_of_rwy = D_cg_north_of_rwy; - FG_D_cg_east_of_rwy = D_cg_east_of_rwy; - FG_D_cg_above_rwy = D_cg_above_rwy; - FG_X_cg_rwy = X_cg_rwy; - FG_Y_cg_rwy = Y_cg_rwy; - FG_H_cg_rwy = H_cg_rwy; - FG_D_pilot_north_of_rwy = D_pilot_north_of_rwy; - FG_D_pilot_east_of_rwy = D_pilot_east_of_rwy; - FG_D_pilot_above_rwy = D_pilot_above_rwy; - FG_X_pilot_rwy = X_pilot_rwy; - FG_Y_pilot_rwy = Y_pilot_rwy; - FG_H_pilot_rwy = H_pilot_rwy; - - return ( 0 ); -} -#endif - /* Set the altitude (force) */ int ls_ForceAltitude(double alt_feet) { Altitude = alt_feet; @@ -927,6 +574,9 @@ int ls_ForceAltitude(double alt_feet) { /* Flight Gear Modification Log * * $Log$ + * Revision 1.24 1998/12/14 13:27:47 curt + * Removed some old, outdated, no longer needed code. + * * Revision 1.23 1998/10/16 23:27:44 curt * C++-ifying. *