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hdw-a339x/src/wasm/fbw_a320/src/model/AutopilotLaws.cpp
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hdw-a339x/src/wasm/fbw_a320/src/model/AutopilotLaws_data.cpp
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hdw-a339x/src/wasm/fbw_a320/src/model/AutopilotLaws_private.h
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| #ifndef RTW_HEADER_AutopilotLaws_private_h_ | ||
| #define RTW_HEADER_AutopilotLaws_private_h_ | ||
| #include "rtwtypes.h" | ||
| #include "AutopilotLaws_types.h" | ||
| #endif | ||
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hdw-a339x/src/wasm/fbw_a320/src/model/AutopilotLaws_types.h
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| #ifndef RTW_HEADER_AutopilotLaws_types_h_ | ||
| #define RTW_HEADER_AutopilotLaws_types_h_ | ||
| #include "rtwtypes.h" | ||
|
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| #ifndef DEFINED_TYPEDEF_FOR_ap_raw_laws_flare_ | ||
| #define DEFINED_TYPEDEF_FOR_ap_raw_laws_flare_ | ||
|
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| struct ap_raw_laws_flare | ||
| { | ||
| boolean_T condition_Flare; | ||
| real_T H_dot_radio_fpm; | ||
| real_T H_dot_c_fpm; | ||
| real_T delta_Theta_H_dot_deg; | ||
| real_T delta_Theta_bz_deg; | ||
| real_T delta_Theta_bx_deg; | ||
| real_T delta_Theta_beta_c_deg; | ||
| }; | ||
|
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| #endif | ||
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| #ifndef DEFINED_TYPEDEF_FOR_ap_raw_time_ | ||
| #define DEFINED_TYPEDEF_FOR_ap_raw_time_ | ||
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| struct ap_raw_time | ||
| { | ||
| real_T dt; | ||
| real_T simulation_time; | ||
| }; | ||
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| #endif | ||
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| #ifndef DEFINED_TYPEDEF_FOR_ap_lat_lon_alt_ | ||
| #define DEFINED_TYPEDEF_FOR_ap_lat_lon_alt_ | ||
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| struct ap_lat_lon_alt | ||
| { | ||
| real_T lat; | ||
| real_T lon; | ||
| real_T alt; | ||
| }; | ||
|
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| #endif | ||
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| #ifndef DEFINED_TYPEDEF_FOR_ap_raw_data_ | ||
| #define DEFINED_TYPEDEF_FOR_ap_raw_data_ | ||
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| struct ap_raw_data | ||
| { | ||
| ap_lat_lon_alt aircraft_position; | ||
| real_T Theta_deg; | ||
| real_T Phi_deg; | ||
| real_T q_rad_s; | ||
| real_T r_rad_s; | ||
| real_T p_rad_s; | ||
| real_T V_ias_kn; | ||
| real_T V_tas_kn; | ||
| real_T V_mach; | ||
| real_T V_gnd_kn; | ||
| real_T alpha_deg; | ||
| real_T beta_deg; | ||
| real_T H_ft; | ||
| real_T H_ind_ft; | ||
| real_T H_radio_ft; | ||
| real_T H_dot_ft_min; | ||
| real_T Psi_magnetic_deg; | ||
| real_T Psi_magnetic_track_deg; | ||
| real_T Psi_true_deg; | ||
| real_T bx_m_s2; | ||
| real_T by_m_s2; | ||
| real_T bz_m_s2; | ||
| boolean_T nav_valid; | ||
| real_T nav_loc_deg; | ||
| real_T nav_gs_deg; | ||
| real_T nav_dme_valid; | ||
| real_T nav_dme_nmi; | ||
| boolean_T nav_loc_valid; | ||
| real_T nav_loc_magvar_deg; | ||
| real_T nav_loc_error_deg; | ||
| ap_lat_lon_alt nav_loc_position; | ||
| boolean_T nav_gs_valid; | ||
| real_T nav_gs_error_deg; | ||
| ap_lat_lon_alt nav_gs_position; | ||
| real_T flight_guidance_xtk_nmi; | ||
| real_T flight_guidance_tae_deg; | ||
| real_T flight_guidance_phi_deg; | ||
| real_T flight_guidance_phi_limit_deg; | ||
| real_T flight_phase; | ||
| real_T V2_kn; | ||
| real_T VAPP_kn; | ||
| real_T VLS_kn; | ||
| real_T VMAX_kn; | ||
| boolean_T is_flight_plan_available; | ||
| real_T altitude_constraint_ft; | ||
| real_T thrust_reduction_altitude; | ||
| real_T thrust_reduction_altitude_go_around; | ||
| real_T acceleration_altitude; | ||
| real_T acceleration_altitude_engine_out; | ||
| real_T acceleration_altitude_go_around; | ||
| real_T acceleration_altitude_go_around_engine_out; | ||
| real_T cruise_altitude; | ||
| real_T gear_strut_compression_1; | ||
| real_T gear_strut_compression_2; | ||
| real_T zeta_pos; | ||
| real_T throttle_lever_1_pos; | ||
| real_T throttle_lever_2_pos; | ||
| real_T flaps_handle_index; | ||
| boolean_T is_engine_operative_1; | ||
| boolean_T is_engine_operative_2; | ||
| real_T altimeter_setting_left_mbar; | ||
| real_T altimeter_setting_right_mbar; | ||
| real_T total_weight_kg; | ||
| }; | ||
|
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| #endif | ||
|
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| #ifndef DEFINED_TYPEDEF_FOR_ap_raw_laws_input_ | ||
| #define DEFINED_TYPEDEF_FOR_ap_raw_laws_input_ | ||
|
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| struct ap_raw_laws_input | ||
| { | ||
| real_T enabled_AP1; | ||
| real_T enabled_AP2; | ||
| real_T lateral_law; | ||
| real_T lateral_mode; | ||
| real_T lateral_mode_armed; | ||
| real_T vertical_law; | ||
| real_T vertical_mode; | ||
| real_T vertical_mode_armed; | ||
| real_T mode_reversion_lateral; | ||
| real_T mode_reversion_vertical; | ||
| real_T mode_reversion_vertical_target_fpm; | ||
| boolean_T mode_reversion_TRK_FPA; | ||
| boolean_T mode_reversion_triple_click; | ||
| boolean_T mode_reversion_fma; | ||
| boolean_T speed_protection_mode; | ||
| real_T autothrust_mode; | ||
| real_T Psi_c_deg; | ||
| real_T H_c_ft; | ||
| real_T H_dot_c_fpm; | ||
| real_T FPA_c_deg; | ||
| real_T V_c_kn; | ||
| boolean_T ALT_soft_mode_active; | ||
| boolean_T ALT_cruise_mode_active; | ||
| boolean_T EXPED_mode_active; | ||
| boolean_T FD_disconnect; | ||
| boolean_T FD_connect; | ||
| boolean_T TCAS_message_disarm; | ||
| boolean_T TCAS_message_RA_inhibit; | ||
| boolean_T TCAS_message_TRK_FPA_deselection; | ||
| }; | ||
|
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| #endif | ||
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| #ifndef DEFINED_TYPEDEF_FOR_ap_laws_input_ | ||
| #define DEFINED_TYPEDEF_FOR_ap_laws_input_ | ||
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| struct ap_laws_input | ||
| { | ||
| ap_raw_time time; | ||
| ap_raw_data data; | ||
| ap_raw_laws_input input; | ||
| }; | ||
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| #endif | ||
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| #ifndef DEFINED_TYPEDEF_FOR_ap_data_ | ||
| #define DEFINED_TYPEDEF_FOR_ap_data_ | ||
|
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| struct ap_data | ||
| { | ||
| ap_lat_lon_alt aircraft_position; | ||
| real_T Theta_deg; | ||
| real_T Phi_deg; | ||
| real_T qk_deg_s; | ||
| real_T rk_deg_s; | ||
| real_T pk_deg_s; | ||
| real_T V_ias_kn; | ||
| real_T V_tas_kn; | ||
| real_T V_mach; | ||
| real_T V_gnd_kn; | ||
| real_T alpha_deg; | ||
| real_T beta_deg; | ||
| real_T H_ft; | ||
| real_T H_ind_ft; | ||
| real_T H_radio_ft; | ||
| real_T H_dot_ft_min; | ||
| real_T Psi_magnetic_deg; | ||
| real_T Psi_magnetic_track_deg; | ||
| real_T Psi_true_deg; | ||
| real_T ax_m_s2; | ||
| real_T ay_m_s2; | ||
| real_T az_m_s2; | ||
| real_T bx_m_s2; | ||
| real_T by_m_s2; | ||
| real_T bz_m_s2; | ||
| boolean_T nav_valid; | ||
| real_T nav_loc_deg; | ||
| real_T nav_gs_deg; | ||
| real_T nav_dme_valid; | ||
| real_T nav_dme_nmi; | ||
| boolean_T nav_loc_valid; | ||
| real_T nav_loc_magvar_deg; | ||
| real_T nav_loc_error_deg; | ||
| ap_lat_lon_alt nav_loc_position; | ||
| boolean_T nav_e_loc_valid; | ||
| real_T nav_e_loc_error_deg; | ||
| boolean_T nav_gs_valid; | ||
| real_T nav_gs_error_deg; | ||
| ap_lat_lon_alt nav_gs_position; | ||
| boolean_T nav_e_gs_valid; | ||
| real_T nav_e_gs_error_deg; | ||
| real_T flight_guidance_xtk_nmi; | ||
| real_T flight_guidance_tae_deg; | ||
| real_T flight_guidance_phi_deg; | ||
| real_T flight_guidance_phi_limit_deg; | ||
| real_T flight_phase; | ||
| real_T V2_kn; | ||
| real_T VAPP_kn; | ||
| real_T VLS_kn; | ||
| real_T VMAX_kn; | ||
| boolean_T is_flight_plan_available; | ||
| real_T altitude_constraint_ft; | ||
| real_T thrust_reduction_altitude; | ||
| real_T thrust_reduction_altitude_go_around; | ||
| real_T acceleration_altitude; | ||
| real_T acceleration_altitude_engine_out; | ||
| real_T acceleration_altitude_go_around; | ||
| real_T acceleration_altitude_go_around_engine_out; | ||
| real_T cruise_altitude; | ||
| real_T on_ground; | ||
| real_T zeta_deg; | ||
| real_T throttle_lever_1_pos; | ||
| real_T throttle_lever_2_pos; | ||
| real_T flaps_handle_index; | ||
| boolean_T is_engine_operative_1; | ||
| boolean_T is_engine_operative_2; | ||
| boolean_T altimeter_setting_changed; | ||
| real_T total_weight_kg; | ||
| }; | ||
|
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| #endif | ||
|
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| #ifndef DEFINED_TYPEDEF_FOR_ap_raw_output_command_ | ||
| #define DEFINED_TYPEDEF_FOR_ap_raw_output_command_ | ||
|
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| struct ap_raw_output_command | ||
| { | ||
| real_T Theta_c_deg; | ||
| real_T Phi_c_deg; | ||
| real_T Beta_c_deg; | ||
| }; | ||
|
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| #endif | ||
|
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| #ifndef DEFINED_TYPEDEF_FOR_ap_raw_output_ | ||
| #define DEFINED_TYPEDEF_FOR_ap_raw_output_ | ||
|
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| struct ap_raw_output | ||
| { | ||
| real_T ap_on; | ||
| real_T Phi_loc_c; | ||
| real_T Nosewheel_c; | ||
| ap_raw_output_command flight_director; | ||
| ap_raw_output_command autopilot; | ||
| ap_raw_laws_flare flare_law; | ||
| }; | ||
|
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| #endif | ||
|
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| #ifndef DEFINED_TYPEDEF_FOR_ap_laws_output_ | ||
| #define DEFINED_TYPEDEF_FOR_ap_laws_output_ | ||
|
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| struct ap_laws_output | ||
| { | ||
| ap_raw_time time; | ||
| ap_data data; | ||
| ap_raw_laws_input input; | ||
| ap_raw_output output; | ||
| }; | ||
|
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| #endif | ||
|
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| #ifndef DEFINED_TYPEDEF_FOR_ap_output_law_ | ||
| #define DEFINED_TYPEDEF_FOR_ap_output_law_ | ||
|
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| struct ap_output_law | ||
| { | ||
| real_T flight_director; | ||
| real_T autopilot; | ||
| }; | ||
|
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| #endif | ||
|
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| #ifndef DEFINED_TYPEDEF_FOR_vertical_mode_ | ||
| #define DEFINED_TYPEDEF_FOR_vertical_mode_ | ||
|
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| enum class vertical_mode | ||
| : int32_T { | ||
| NONE = 0, | ||
| ALT = 10, | ||
| ALT_CPT = 11, | ||
| OP_CLB = 12, | ||
| OP_DES = 13, | ||
| VS = 14, | ||
| FPA = 15, | ||
| ALT_CST = 20, | ||
| ALT_CST_CPT = 21, | ||
| CLB = 22, | ||
| DES = 23, | ||
| FINAL_DES = 24, | ||
| GS_CPT = 30, | ||
| GS_TRACK = 31, | ||
| LAND = 32, | ||
| FLARE = 33, | ||
| ROLL_OUT = 34, | ||
| SRS = 40, | ||
| SRS_GA = 41, | ||
| TCAS = 50 | ||
| }; | ||
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| #endif | ||
|
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| #ifndef DEFINED_TYPEDEF_FOR_lateral_mode_ | ||
| #define DEFINED_TYPEDEF_FOR_lateral_mode_ | ||
|
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| enum class lateral_mode | ||
| : int32_T { | ||
| NONE = 0, | ||
| HDG = 10, | ||
| TRACK = 11, | ||
| NAV = 20, | ||
| LOC_CPT = 30, | ||
| LOC_TRACK = 31, | ||
| LAND = 32, | ||
| FLARE = 33, | ||
| ROLL_OUT = 34, | ||
| RWY = 40, | ||
| RWY_TRACK = 41, | ||
| GA_TRACK = 50 | ||
| }; | ||
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| #endif | ||
| #endif | ||
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