X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=src%2FFDM%2FUIUCModel%2Fuiuc_menu_engine.cpp;h=d2b1e431a6365e28db01138afd79ecadc3361422;hb=c62b0044380eb0387c447cc33660f74b02cbbce4;hp=96ede0e3650378f8d3cf1e5a6d755558ea046246;hpb=667e64e1ebc86a0c53112b92b53475898f315c36;p=flightgear.git diff --git a/src/FDM/UIUCModel/uiuc_menu_engine.cpp b/src/FDM/UIUCModel/uiuc_menu_engine.cpp index 96ede0e36..d2b1e431a 100644 --- a/src/FDM/UIUCModel/uiuc_menu_engine.cpp +++ b/src/FDM/UIUCModel/uiuc_menu_engine.cpp @@ -46,10 +46,10 @@ ---------------------------------------------------------------------- CALLS TO: check_float() if needed - d_2_to_3() if needed - d_1_to_2() if needed - i_1_to_2() if needed - d_1_to_1() if needed + d_2_to_3() if needed + d_1_to_2() if needed + i_1_to_2() if needed + d_1_to_1() if needed ---------------------------------------------------------------------- @@ -88,11 +88,11 @@ using std::exit; #endif void parse_engine( const string& linetoken2, const string& linetoken3, - const string& linetoken4, const string& linetoken5, - const string& linetoken6, const string& linetoken7, - const string& linetoken8, const string& linetoken9, - const string& linetoken10,const string& aircraft_directory, - LIST command_line ) { + const string& linetoken4, const string& linetoken5, + const string& linetoken6, const string& linetoken7, + const string& linetoken8, const string& linetoken9, + const string& linetoken10,const string& aircraft_directory, + LIST command_line ) { double token_value; int token_value_convert1, token_value_convert2; istringstream token3(linetoken3.c_str()); @@ -107,375 +107,375 @@ void parse_engine( const string& linetoken2, const string& linetoken3, switch(engine_map[linetoken2]) { case simpleSingle_flag: - { - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - - simpleSingleMaxThrust = token_value; - engineParts -> storeCommands (*command_line); - break; - } + { + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + + simpleSingleMaxThrust = token_value; + engineParts -> storeCommands (*command_line); + break; + } case simpleSingleModel_flag: - { - simpleSingleModel = true; - /* input the thrust at zero speed */ - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - t_v0 = token_value; - /* input slope of thrust at speed for which thrust is zero */ - if (check_float(linetoken4)) - token4 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - dtdv_t0 = token_value; - /* input speed at which thrust is zero */ - if (check_float(linetoken5)) - token5 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - v_t0 = token_value; - dtdvvt = -dtdv_t0 * v_t0 / t_v0; - engineParts -> storeCommands (*command_line); - break; - } + { + simpleSingleModel = true; + /* input the thrust at zero speed */ + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + t_v0 = token_value; + /* input slope of thrust at speed for which thrust is zero */ + if (check_float(linetoken4)) + token4 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + dtdv_t0 = token_value; + /* input speed at which thrust is zero */ + if (check_float(linetoken5)) + token5 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + v_t0 = token_value; + dtdvvt = -dtdv_t0 * v_t0 / t_v0; + engineParts -> storeCommands (*command_line); + break; + } case c172_flag: - { - engineParts -> storeCommands (*command_line); - break; - } + { + engineParts -> storeCommands (*command_line); + break; + } case cherokee_flag: - { - engineParts -> storeCommands (*command_line); - break; - } + { + engineParts -> storeCommands (*command_line); + break; + } case Throttle_pct_input_flag: - { - Throttle_pct_input = true; - Throttle_pct_input_file = aircraft_directory + linetoken3; - token4 >> token_value_convert1; - token5 >> token_value_convert2; - convert_y = uiuc_convert(token_value_convert1); - convert_x = uiuc_convert(token_value_convert2); - uiuc_1DdataFileReader(Throttle_pct_input_file, - Throttle_pct_input_timeArray, - Throttle_pct_input_dTArray, - Throttle_pct_input_ntime); - token6 >> token_value; - Throttle_pct_input_startTime = token_value; - break; - } + { + Throttle_pct_input = true; + Throttle_pct_input_file = aircraft_directory + linetoken3; + token4 >> token_value_convert1; + token5 >> token_value_convert2; + convert_y = uiuc_convert(token_value_convert1); + convert_x = uiuc_convert(token_value_convert2); + uiuc_1DdataFileReader(Throttle_pct_input_file, + Throttle_pct_input_timeArray, + Throttle_pct_input_dTArray, + Throttle_pct_input_ntime); + token6 >> token_value; + Throttle_pct_input_startTime = token_value; + break; + } case gyroForce_Q_body_flag: - { - /* include gyroscopic forces due to pitch */ - gyroForce_Q_body = true; - break; - } + { + /* include gyroscopic forces due to pitch */ + gyroForce_Q_body = true; + break; + } case gyroForce_R_body_flag: - { - /* include gyroscopic forces due to yaw */ - gyroForce_R_body = true; - break; - } + { + /* include gyroscopic forces due to yaw */ + gyroForce_R_body = true; + break; + } case slipstream_effects_flag: - { - // include slipstream effects - b_slipstreamEffects = true; - if (!simpleSingleModel) - uiuc_warnings_errors(3, *command_line); - break; - } + { + // include slipstream effects + b_slipstreamEffects = true; + if (!simpleSingleModel) + uiuc_warnings_errors(3, *command_line); + break; + } case propDia_flag: - { - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - propDia = token_value; - break; - } + { + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + propDia = token_value; + break; + } case eta_q_Cm_q_flag: - { - // include slipstream effects due to Cm_q - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_Cm_q_fac = token_value; - if (eta_q_Cm_q_fac == 0.0) {eta_q_Cm_q_fac = 1.0;} - break; - } + { + // include slipstream effects due to Cm_q + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_Cm_q_fac = token_value; + if (eta_q_Cm_q_fac == 0.0) {eta_q_Cm_q_fac = 1.0;} + break; + } case eta_q_Cm_adot_flag: - { - // include slipstream effects due to Cm_adot - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_Cm_adot_fac = token_value; - if (eta_q_Cm_adot_fac == 0.0) {eta_q_Cm_adot_fac = 1.0;} - break; - } + { + // include slipstream effects due to Cm_adot + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_Cm_adot_fac = token_value; + if (eta_q_Cm_adot_fac == 0.0) {eta_q_Cm_adot_fac = 1.0;} + break; + } case eta_q_Cmfade_flag: - { - // include slipstream effects due to Cmfade - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_Cmfade_fac = token_value; - if (eta_q_Cmfade_fac == 0.0) {eta_q_Cmfade_fac = 1.0;} - break; - } + { + // include slipstream effects due to Cmfade + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_Cmfade_fac = token_value; + if (eta_q_Cmfade_fac == 0.0) {eta_q_Cmfade_fac = 1.0;} + break; + } case eta_q_Cm_de_flag: - { - // include slipstream effects due to Cmfade - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_Cm_de_fac = token_value; - if (eta_q_Cm_de_fac == 0.0) {eta_q_Cm_de_fac = 1.0;} - break; - } + { + // include slipstream effects due to Cmfade + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_Cm_de_fac = token_value; + if (eta_q_Cm_de_fac == 0.0) {eta_q_Cm_de_fac = 1.0;} + break; + } case eta_q_Cl_beta_flag: - { - // include slipstream effects due to Cl_beta - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_Cl_beta_fac = token_value; - if (eta_q_Cl_beta_fac == 0.0) {eta_q_Cl_beta_fac = 1.0;} - break; - } + { + // include slipstream effects due to Cl_beta + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_Cl_beta_fac = token_value; + if (eta_q_Cl_beta_fac == 0.0) {eta_q_Cl_beta_fac = 1.0;} + break; + } case eta_q_Cl_p_flag: - { - // include slipstream effects due to Cl_p - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_Cl_p_fac = token_value; - if (eta_q_Cl_p_fac == 0.0) {eta_q_Cl_p_fac = 1.0;} - break; - } + { + // include slipstream effects due to Cl_p + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_Cl_p_fac = token_value; + if (eta_q_Cl_p_fac == 0.0) {eta_q_Cl_p_fac = 1.0;} + break; + } case eta_q_Cl_r_flag: - { - // include slipstream effects due to Cl_r - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_Cl_r_fac = token_value; - if (eta_q_Cl_r_fac == 0.0) {eta_q_Cl_r_fac = 1.0;} - break; - } + { + // include slipstream effects due to Cl_r + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_Cl_r_fac = token_value; + if (eta_q_Cl_r_fac == 0.0) {eta_q_Cl_r_fac = 1.0;} + break; + } case eta_q_Cl_dr_flag: - { - // include slipstream effects due to Cl_dr - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_Cl_dr_fac = token_value; - if (eta_q_Cl_dr_fac == 0.0) {eta_q_Cl_dr_fac = 1.0;} - break; - } + { + // include slipstream effects due to Cl_dr + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_Cl_dr_fac = token_value; + if (eta_q_Cl_dr_fac == 0.0) {eta_q_Cl_dr_fac = 1.0;} + break; + } case eta_q_CY_beta_flag: - { - // include slipstream effects due to CY_beta - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_CY_beta_fac = token_value; - if (eta_q_CY_beta_fac == 0.0) {eta_q_CY_beta_fac = 1.0;} - break; - } + { + // include slipstream effects due to CY_beta + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_CY_beta_fac = token_value; + if (eta_q_CY_beta_fac == 0.0) {eta_q_CY_beta_fac = 1.0;} + break; + } case eta_q_CY_p_flag: - { - // include slipstream effects due to CY_p - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_CY_p_fac = token_value; - if (eta_q_CY_p_fac == 0.0) {eta_q_CY_p_fac = 1.0;} - break; - } + { + // include slipstream effects due to CY_p + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_CY_p_fac = token_value; + if (eta_q_CY_p_fac == 0.0) {eta_q_CY_p_fac = 1.0;} + break; + } case eta_q_CY_r_flag: - { - // include slipstream effects due to CY_r - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_CY_r_fac = token_value; - if (eta_q_CY_r_fac == 0.0) {eta_q_CY_r_fac = 1.0;} - break; - } + { + // include slipstream effects due to CY_r + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_CY_r_fac = token_value; + if (eta_q_CY_r_fac == 0.0) {eta_q_CY_r_fac = 1.0;} + break; + } case eta_q_CY_dr_flag: - { - // include slipstream effects due to CY_dr - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_CY_dr_fac = token_value; - if (eta_q_CY_dr_fac == 0.0) {eta_q_CY_dr_fac = 1.0;} - break; - } + { + // include slipstream effects due to CY_dr + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_CY_dr_fac = token_value; + if (eta_q_CY_dr_fac == 0.0) {eta_q_CY_dr_fac = 1.0;} + break; + } case eta_q_Cn_beta_flag: - { - // include slipstream effects due to Cn_beta - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_Cn_beta_fac = token_value; - if (eta_q_Cn_beta_fac == 0.0) {eta_q_Cn_beta_fac = 1.0;} - break; - } + { + // include slipstream effects due to Cn_beta + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_Cn_beta_fac = token_value; + if (eta_q_Cn_beta_fac == 0.0) {eta_q_Cn_beta_fac = 1.0;} + break; + } case eta_q_Cn_p_flag: - { - // include slipstream effects due to Cn_p - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_Cn_p_fac = token_value; - if (eta_q_Cn_p_fac == 0.0) {eta_q_Cn_p_fac = 1.0;} - break; - } + { + // include slipstream effects due to Cn_p + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_Cn_p_fac = token_value; + if (eta_q_Cn_p_fac == 0.0) {eta_q_Cn_p_fac = 1.0;} + break; + } case eta_q_Cn_r_flag: - { - // include slipstream effects due to Cn_r - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_Cn_r_fac = token_value; - if (eta_q_Cn_r_fac == 0.0) {eta_q_Cn_r_fac = 1.0;} - break; - } + { + // include slipstream effects due to Cn_r + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_Cn_r_fac = token_value; + if (eta_q_Cn_r_fac == 0.0) {eta_q_Cn_r_fac = 1.0;} + break; + } case eta_q_Cn_dr_flag: - { - // include slipstream effects due to Cn_dr - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - eta_q_Cn_dr_fac = token_value; - if (eta_q_Cn_dr_fac == 0.0) {eta_q_Cn_dr_fac = 1.0;} - break; - } + { + // include slipstream effects due to Cn_dr + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + eta_q_Cn_dr_fac = token_value; + if (eta_q_Cn_dr_fac == 0.0) {eta_q_Cn_dr_fac = 1.0;} + break; + } case omega_flag: - { - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - minOmega = token_value; - if (check_float(linetoken4)) - token4 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - maxOmega = token_value; - break; - } + { + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + minOmega = token_value; + if (check_float(linetoken4)) + token4 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + maxOmega = token_value; + break; + } case omegaRPM_flag: - { - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - minOmegaRPM = token_value; - minOmega = minOmegaRPM * 2.0 * LS_PI / 60; - if (check_float(linetoken4)) - token4 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - maxOmegaRPM = token_value; - maxOmega = maxOmegaRPM * 2.0 * LS_PI / 60; - break; - } + { + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + minOmegaRPM = token_value; + minOmega = minOmegaRPM * 2.0 * LS_PI / 60; + if (check_float(linetoken4)) + token4 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + maxOmegaRPM = token_value; + maxOmega = maxOmegaRPM * 2.0 * LS_PI / 60; + break; + } case polarInertia_flag: - { - if (check_float(linetoken3)) - token3 >> token_value; - else - uiuc_warnings_errors(1, *command_line); - polarInertia = token_value; - break; - } + { + if (check_float(linetoken3)) + token3 >> token_value; + else + uiuc_warnings_errors(1, *command_line); + polarInertia = token_value; + break; + } case forcemom_flag: - { - engineParts -> storeCommands (*command_line); - break; - } + { + engineParts -> storeCommands (*command_line); + break; + } case Xp_input_flag: - { - Xp_input = true; - Xp_input_file = aircraft_directory + linetoken3; - token4 >> token_value_convert1; - token5 >> token_value_convert2; - convert_y = uiuc_convert(token_value_convert1); - convert_x = uiuc_convert(token_value_convert2); - uiuc_1DdataFileReader(Xp_input_file, - Xp_input_timeArray, - Xp_input_XpArray, - Xp_input_ntime); - token6 >> token_value; - Xp_input_startTime = token_value; - break; - } + { + Xp_input = true; + Xp_input_file = aircraft_directory + linetoken3; + token4 >> token_value_convert1; + token5 >> token_value_convert2; + convert_y = uiuc_convert(token_value_convert1); + convert_x = uiuc_convert(token_value_convert2); + uiuc_1DdataFileReader(Xp_input_file, + Xp_input_timeArray, + Xp_input_XpArray, + Xp_input_ntime); + token6 >> token_value; + Xp_input_startTime = token_value; + break; + } case Zp_input_flag: - { - Zp_input = true; - Zp_input_file = aircraft_directory + linetoken3; - token4 >> token_value_convert1; - token5 >> token_value_convert2; - convert_y = uiuc_convert(token_value_convert1); - convert_x = uiuc_convert(token_value_convert2); - uiuc_1DdataFileReader(Zp_input_file, - Zp_input_timeArray, - Zp_input_ZpArray, - Zp_input_ntime); - token6 >> token_value; - Zp_input_startTime = token_value; - break; - } + { + Zp_input = true; + Zp_input_file = aircraft_directory + linetoken3; + token4 >> token_value_convert1; + token5 >> token_value_convert2; + convert_y = uiuc_convert(token_value_convert1); + convert_x = uiuc_convert(token_value_convert2); + uiuc_1DdataFileReader(Zp_input_file, + Zp_input_timeArray, + Zp_input_ZpArray, + Zp_input_ntime); + token6 >> token_value; + Zp_input_startTime = token_value; + break; + } case Mp_input_flag: - { - Mp_input = true; - Mp_input_file = aircraft_directory + linetoken3; - token4 >> token_value_convert1; - token5 >> token_value_convert2; - convert_y = uiuc_convert(token_value_convert1); - convert_x = uiuc_convert(token_value_convert2); - uiuc_1DdataFileReader(Mp_input_file, - Mp_input_timeArray, - Mp_input_MpArray, - Mp_input_ntime); - token6 >> token_value; - Mp_input_startTime = token_value; - break; - } + { + Mp_input = true; + Mp_input_file = aircraft_directory + linetoken3; + token4 >> token_value_convert1; + token5 >> token_value_convert2; + convert_y = uiuc_convert(token_value_convert1); + convert_x = uiuc_convert(token_value_convert2); + uiuc_1DdataFileReader(Mp_input_file, + Mp_input_timeArray, + Mp_input_MpArray, + Mp_input_ntime); + token6 >> token_value; + Mp_input_startTime = token_value; + break; + } default: - { - if (ignore_unknown_keywords) { - // do nothing - } else { - // print error message - uiuc_warnings_errors(2, *command_line); - } - break; - } + { + if (ignore_unknown_keywords) { + // do nothing + } else { + // print error message + uiuc_warnings_errors(2, *command_line); + } + break; + } }; }