// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- #ifndef PARAMETERS_H #define PARAMETERS_H #include // Global parameter class. // class Parameters { public: // The version of the layout as described by the parameter enum. // // When changing the parameter enum in an incompatible fashion, this // value should be incremented by one. // // The increment will prevent old parameters from being used incorrectly // by newer code. // static const uint16_t k_format_version = 14; // The parameter software_type is set up solely for ground station use // and identifies the software type (eg ArduPilotMega versus ArduCopterMega) // GCS will interpret values 0-9 as ArduPilotMega. Developers may use // values within that range to identify different branches. // static const uint16_t k_software_type = 20; // 0 for APM trunk enum { // Layout version number, always key zero. // k_param_format_version = 0, k_param_software_type, // Misc // k_param_auto_trim, k_param_switch_enable, k_param_log_bitmask, k_param_mix_mode, // unused k_param_reverse_elevons, // unused k_param_reverse_ch1_elevon, // unused k_param_reverse_ch2_elevon, // unused k_param_flap_1_percent, // unused k_param_flap_1_speed, // unused k_param_flap_2_percent, // unused k_param_flap_2_speed, // unused k_param_num_resets, k_param_log_last_filenumber, // *** Deprecated - remove with next eeprom number change k_param_reset_switch_chan, k_param_manual_level, k_param_ins, // libraries/AP_InertialSensor variables // 110: Telemetry control // k_param_gcs0 = 110, // stream rates for port0 k_param_gcs3, // stream rates for port3 k_param_sysid_this_mav, k_param_sysid_my_gcs, k_param_serial3_baud, k_param_telem_delay, // 120: Fly-by-wire control // k_param_flybywire_airspeed_min = 120, k_param_flybywire_airspeed_max, k_param_FBWB_min_altitude, // 0=disabled, minimum value for altitude in cm (for first time try 30 meters = 3000 cm) // // 130: Sensor parameters // k_param_imu = 130, k_param_altitude_mix, // sensor calibration k_param_airspeed_ratio, k_param_ground_temperature, k_param_ground_pressure, k_param_compass_enabled, k_param_compass, k_param_battery_monitoring, k_param_volt_div_ratio, k_param_curr_amp_per_volt, k_param_input_voltage, k_param_pack_capacity, k_param_airspeed_offset, #if HIL_MODE != HIL_MODE_ATTITUDE #if CONFIG_SONAR == ENABLED k_param_sonar_enabled, k_param_sonar_type, #endif #endif k_param_ahrs, // AHRS group // // 150: Navigation parameters // k_param_crosstrack_gain = 150, k_param_crosstrack_entry_angle, k_param_roll_limit, k_param_pitch_limit_max, k_param_pitch_limit_min, k_param_airspeed_cruise, k_param_min_gndspeed, k_param_ch7_option, // // 160: Radio settings // k_param_channel_roll = 160, k_param_channel_pitch, k_param_channel_throttle, k_param_channel_rudder, k_param_rc_5, k_param_rc_6, k_param_rc_7, k_param_rc_8, k_param_throttle_min, k_param_throttle_max, k_param_throttle_fs_enabled, // 170 k_param_throttle_fs_value, k_param_throttle_cruise, k_param_short_fs_action, k_param_long_fs_action, k_param_gcs_heartbeat_fs_enabled, k_param_throttle_slewrate, // ************************************************************ // 180: APMrover parameters - JLN update k_param_closed_loop_nav, // unused k_param_auto_wp_radius, k_param_sonar_trigger, k_param_turn_gain, k_param_booster, // ************************************************************ // // 200: Feed-forward gains // k_param_kff_pitch_compensation = 200, // unused k_param_kff_rudder_mix, // unused k_param_kff_pitch_to_throttle, // unused k_param_kff_throttle_to_pitch, // unused // // 210: flight modes // k_param_flight_mode_channel = 210, k_param_flight_mode1, k_param_flight_mode2, k_param_flight_mode3, k_param_flight_mode4, k_param_flight_mode5, k_param_flight_mode6, // // 220: Waypoint data // k_param_waypoint_mode = 220, k_param_command_total, k_param_command_index, k_param_waypoint_radius, k_param_loiter_radius, // unused k_param_fence_action, k_param_fence_total, k_param_fence_channel, k_param_fence_minalt, k_param_fence_maxalt, // other objects k_param_sitl = 230, // // 240: PID Controllers // // Heading-to-roll PID: // heading error from command to roll command deviation from trim // (bank to turn strategy) // k_param_pidNavRoll = 240, // Roll-to-servo PID: // roll error from command to roll servo deviation from trim // (tracks commanded bank angle) // k_param_pidServoRoll, // // Pitch control // // Pitch-to-servo PID: // pitch error from command to pitch servo deviation from trim // (front-side strategy) // k_param_pidServoPitch, // Airspeed-to-pitch PID: // airspeed error from command to pitch servo deviation from trim // (back-side strategy) // k_param_pidNavPitchAirspeed, // // Yaw control // // Yaw-to-servo PID: // yaw rate error from command to yaw servo deviation from trim // (stabilizes dutch roll) // k_param_pidServoRudder, // // Throttle control // // Energy-to-throttle PID: // total energy error from command to throttle servo deviation from trim // (throttle back-side strategy alternative) // k_param_pidTeThrottle, // Altitude-to-pitch PID: // altitude error from command to pitch servo deviation from trim // (throttle front-side strategy alternative) // k_param_pidNavPitchAltitude, // 254,255: reserved }; AP_Int16 format_version; AP_Int8 software_type; // Telemetry control // AP_Int16 sysid_this_mav; AP_Int16 sysid_my_gcs; AP_Int8 serial3_baud; AP_Int8 telem_delay; // Crosstrack navigation // AP_Float crosstrack_gain; AP_Int16 crosstrack_entry_angle; // Estimation // AP_Float altitude_mix; AP_Float airspeed_ratio; AP_Int16 airspeed_offset; // Waypoints // AP_Int8 waypoint_mode; AP_Int8 command_total; AP_Int8 command_index; AP_Int8 waypoint_radius; // Fly-by-wire // AP_Int8 flybywire_airspeed_min; AP_Int8 flybywire_airspeed_max; AP_Int16 FBWB_min_altitude; // Throttle // AP_Int8 throttle_min; AP_Int8 throttle_max; AP_Int8 throttle_slewrate; AP_Int8 throttle_fs_enabled; AP_Int16 throttle_fs_value; AP_Int8 throttle_cruise; // Failsafe AP_Int8 short_fs_action; AP_Int8 long_fs_action; AP_Int8 gcs_heartbeat_fs_enabled; // Flight modes // AP_Int8 flight_mode_channel; AP_Int8 flight_mode1; AP_Int8 flight_mode2; AP_Int8 flight_mode3; AP_Int8 flight_mode4; AP_Int8 flight_mode5; AP_Int8 flight_mode6; // Navigational maneuvering limits // AP_Int16 roll_limit; AP_Int16 pitch_limit_max; AP_Int16 pitch_limit_min; // Misc // AP_Int8 auto_trim; AP_Int16 num_resets; AP_Int16 log_bitmask; AP_Int16 log_last_filenumber; // *** Deprecated - remove with next eeprom number change AP_Int8 reset_switch_chan; AP_Int8 manual_level; AP_Int16 airspeed_cruise; AP_Int16 min_gndspeed; AP_Int8 ch7_option; AP_Int16 ground_temperature; AP_Int32 ground_pressure; AP_Int8 compass_enabled; AP_Int16 angle_of_attack; AP_Int8 battery_monitoring; // 0=disabled, 3=voltage only, 4=voltage and current AP_Float volt_div_ratio; AP_Float curr_amp_per_volt; AP_Float input_voltage; AP_Int16 pack_capacity; // Battery pack capacity less reserve #if HIL_MODE != HIL_MODE_ATTITUDE #if CONFIG_SONAR == ENABLED AP_Int8 sonar_enabled; AP_Int8 sonar_type; // 0 = XL, 1 = LV, // 2 = XLL (XL with 10m range) // 3 = HRLV #endif #endif // ************ ThermoPilot parameters ************************ // - JLN update AP_Int8 auto_wp_radius; AP_Int16 sonar_trigger; AP_Int16 turn_gain; AP_Int8 booster; // ************************************************************ // RC channels RC_Channel channel_roll; RC_Channel channel_pitch; RC_Channel channel_throttle; RC_Channel channel_rudder; RC_Channel_aux rc_5; RC_Channel_aux rc_6; RC_Channel_aux rc_7; RC_Channel_aux rc_8; // PID controllers // PID pidNavRoll; PID pidServoRoll; PID pidServoPitch; PID pidNavPitchAirspeed; PID pidServoRudder; PID pidTeThrottle; PID pidNavPitchAltitude; Parameters() : // RC channels channel_roll(CH_1), channel_pitch(CH_2), channel_throttle(CH_3), channel_rudder(CH_4), rc_5(CH_5), rc_6(CH_6), rc_7(CH_7), rc_8(CH_8), // PID controller initial P initial I initial D initial imax //----------------------------------------------------------------------------------- pidNavRoll (NAV_ROLL_P, NAV_ROLL_I, NAV_ROLL_D, NAV_ROLL_INT_MAX_CENTIDEGREE), pidServoRoll (SERVO_ROLL_P, SERVO_ROLL_I, SERVO_ROLL_D, SERVO_ROLL_INT_MAX_CENTIDEGREE), pidServoPitch (SERVO_PITCH_P, SERVO_PITCH_I, SERVO_PITCH_D, SERVO_PITCH_INT_MAX_CENTIDEGREE), pidNavPitchAirspeed (NAV_PITCH_ASP_P, NAV_PITCH_ASP_I, NAV_PITCH_ASP_D, NAV_PITCH_ASP_INT_MAX_CMSEC), pidServoRudder (SERVO_YAW_P, SERVO_YAW_I, SERVO_YAW_D, SERVO_YAW_INT_MAX), pidTeThrottle (THROTTLE_TE_P, THROTTLE_TE_I, THROTTLE_TE_D, THROTTLE_TE_INT_MAX), pidNavPitchAltitude (NAV_PITCH_ALT_P, NAV_PITCH_ALT_I, NAV_PITCH_ALT_D, NAV_PITCH_ALT_INT_MAX_CM) {} }; extern const AP_Param::Info var_info[]; #endif // PARAMETERS_H