#include "Copter.h" #if LOGGING_ENABLED == ENABLED // Code to Write and Read packets from AP_Logger log memory // Code to interact with the user to dump or erase logs struct PACKED log_Control_Tuning { LOG_PACKET_HEADER; uint64_t time_us; float throttle_in; float angle_boost; float throttle_out; float throttle_hover; float desired_alt; float inav_alt; int32_t baro_alt; float desired_rangefinder_alt; float rangefinder_alt; float terr_alt; int16_t target_climb_rate; int16_t climb_rate; }; // Write a control tuning packet void Copter::Log_Write_Control_Tuning() { // get terrain altitude float terr_alt = 0.0f; #if AP_TERRAIN_AVAILABLE && AC_TERRAIN if (!terrain.height_above_terrain(terr_alt, true)) { terr_alt = logger.quiet_nan(); } #endif float des_alt_m = 0.0f; int16_t target_climb_rate_cms = 0; if (!flightmode->has_manual_throttle()) { des_alt_m = pos_control->get_alt_target() / 100.0f; target_climb_rate_cms = pos_control->get_vel_target_z(); } // get surface tracking alts float desired_rangefinder_alt; if (!surface_tracking.get_target_dist_for_logging(desired_rangefinder_alt)) { desired_rangefinder_alt = AP::logger().quiet_nan(); } struct log_Control_Tuning pkt = { LOG_PACKET_HEADER_INIT(LOG_CONTROL_TUNING_MSG), time_us : AP_HAL::micros64(), throttle_in : attitude_control->get_throttle_in(), angle_boost : attitude_control->angle_boost(), throttle_out : motors->get_throttle(), throttle_hover : motors->get_throttle_hover(), desired_alt : des_alt_m, inav_alt : inertial_nav.get_altitude() / 100.0f, baro_alt : baro_alt, desired_rangefinder_alt : desired_rangefinder_alt, rangefinder_alt : surface_tracking.get_dist_for_logging(), terr_alt : terr_alt, target_climb_rate : target_climb_rate_cms, climb_rate : int16_t(inertial_nav.get_velocity_z()) // float -> int16_t }; logger.WriteBlock(&pkt, sizeof(pkt)); } // Write an attitude packet void Copter::Log_Write_Attitude() { Vector3f targets = attitude_control->get_att_target_euler_cd(); targets.z = wrap_360_cd(targets.z); logger.Write_Attitude(targets); logger.Write_Rate(ahrs_view, *motors, *attitude_control, *pos_control); if (should_log(MASK_LOG_PID)) { logger.Write_PID(LOG_PIDR_MSG, attitude_control->get_rate_roll_pid().get_pid_info()); logger.Write_PID(LOG_PIDP_MSG, attitude_control->get_rate_pitch_pid().get_pid_info()); logger.Write_PID(LOG_PIDY_MSG, attitude_control->get_rate_yaw_pid().get_pid_info()); logger.Write_PID(LOG_PIDA_MSG, pos_control->get_accel_z_pid().get_pid_info() ); } } // Write an EKF and POS packet void Copter::Log_Write_EKF_POS() { AP::ahrs_navekf().Log_Write(); logger.Write_AHRS2(); #if CONFIG_HAL_BOARD == HAL_BOARD_SITL sitl.Log_Write_SIMSTATE(); #endif logger.Write_POS(); } struct PACKED log_MotBatt { LOG_PACKET_HEADER; uint64_t time_us; float lift_max; float bat_volt; float bat_res; float th_limit; }; // Write an rate packet void Copter::Log_Write_MotBatt() { #if FRAME_CONFIG != HELI_FRAME struct log_MotBatt pkt_mot = { LOG_PACKET_HEADER_INIT(LOG_MOTBATT_MSG), time_us : AP_HAL::micros64(), lift_max : (float)(motors->get_lift_max()), bat_volt : (float)(motors->get_batt_voltage_filt()), bat_res : (float)(battery.get_resistance()), th_limit : (float)(motors->get_throttle_limit()) }; logger.WriteBlock(&pkt_mot, sizeof(pkt_mot)); #endif } struct PACKED log_Data_Int16t { LOG_PACKET_HEADER; uint64_t time_us; uint8_t id; int16_t data_value; }; // Write an int16_t data packet UNUSED_FUNCTION void Copter::Log_Write_Data(LogDataID id, int16_t value) { if (should_log(MASK_LOG_ANY)) { struct log_Data_Int16t pkt = { LOG_PACKET_HEADER_INIT(LOG_DATA_INT16_MSG), time_us : AP_HAL::micros64(), id : (uint8_t)id, data_value : value }; logger.WriteCriticalBlock(&pkt, sizeof(pkt)); } } struct PACKED log_Data_UInt16t { LOG_PACKET_HEADER; uint64_t time_us; uint8_t id; uint16_t data_value; }; // Write an uint16_t data packet UNUSED_FUNCTION void Copter::Log_Write_Data(LogDataID id, uint16_t value) { if (should_log(MASK_LOG_ANY)) { struct log_Data_UInt16t pkt = { LOG_PACKET_HEADER_INIT(LOG_DATA_UINT16_MSG), time_us : AP_HAL::micros64(), id : (uint8_t)id, data_value : value }; logger.WriteCriticalBlock(&pkt, sizeof(pkt)); } } struct PACKED log_Data_Int32t { LOG_PACKET_HEADER; uint64_t time_us; uint8_t id; int32_t data_value; }; // Write an int32_t data packet void Copter::Log_Write_Data(LogDataID id, int32_t value) { if (should_log(MASK_LOG_ANY)) { struct log_Data_Int32t pkt = { LOG_PACKET_HEADER_INIT(LOG_DATA_INT32_MSG), time_us : AP_HAL::micros64(), id : (uint8_t)id, data_value : value }; logger.WriteCriticalBlock(&pkt, sizeof(pkt)); } } struct PACKED log_Data_UInt32t { LOG_PACKET_HEADER; uint64_t time_us; uint8_t id; uint32_t data_value; }; // Write a uint32_t data packet void Copter::Log_Write_Data(LogDataID id, uint32_t value) { if (should_log(MASK_LOG_ANY)) { struct log_Data_UInt32t pkt = { LOG_PACKET_HEADER_INIT(LOG_DATA_UINT32_MSG), time_us : AP_HAL::micros64(), id : (uint8_t)id, data_value : value }; logger.WriteCriticalBlock(&pkt, sizeof(pkt)); } } struct PACKED log_Data_Float { LOG_PACKET_HEADER; uint64_t time_us; uint8_t id; float data_value; }; // Write a float data packet UNUSED_FUNCTION void Copter::Log_Write_Data(LogDataID id, float value) { if (should_log(MASK_LOG_ANY)) { struct log_Data_Float pkt = { LOG_PACKET_HEADER_INIT(LOG_DATA_FLOAT_MSG), time_us : AP_HAL::micros64(), id : (uint8_t)id, data_value : value }; logger.WriteCriticalBlock(&pkt, sizeof(pkt)); } } struct PACKED log_ParameterTuning { LOG_PACKET_HEADER; uint64_t time_us; uint8_t parameter; // parameter we are tuning, e.g. 39 is CH6_CIRCLE_RATE float tuning_value; // normalized value used inside tuning() function float tuning_min; // tuning minimum value float tuning_max; // tuning maximum value }; void Copter::Log_Write_Parameter_Tuning(uint8_t param, float tuning_val, float tune_min, float tune_max) { struct log_ParameterTuning pkt_tune = { LOG_PACKET_HEADER_INIT(LOG_PARAMTUNE_MSG), time_us : AP_HAL::micros64(), parameter : param, tuning_value : tuning_val, tuning_min : tune_min, tuning_max : tune_max }; logger.WriteBlock(&pkt_tune, sizeof(pkt_tune)); } // logs when baro or compass becomes unhealthy void Copter::Log_Sensor_Health() { // check baro if (sensor_health.baro != barometer.healthy()) { sensor_health.baro = barometer.healthy(); AP::logger().Write_Error(LogErrorSubsystem::BARO, (sensor_health.baro ? LogErrorCode::ERROR_RESOLVED : LogErrorCode::UNHEALTHY)); } // check compass if (sensor_health.compass != compass.healthy()) { sensor_health.compass = compass.healthy(); AP::logger().Write_Error(LogErrorSubsystem::COMPASS, (sensor_health.compass ? LogErrorCode::ERROR_RESOLVED : LogErrorCode::UNHEALTHY)); } // check primary GPS if (sensor_health.primary_gps != gps.primary_sensor()) { sensor_health.primary_gps = gps.primary_sensor(); AP::logger().Write_Event(LogEvent::GPS_PRIMARY_CHANGED); } } struct PACKED log_SysIdD { LOG_PACKET_HEADER; uint64_t time_us; float waveform_time; float waveform_sample; float waveform_freq; float angle_x; float angle_y; float angle_z; float accel_x; float accel_y; float accel_z; }; // Write an rate packet void Copter::Log_Write_SysID_Data(float waveform_time, float waveform_sample, float waveform_freq, float angle_x, float angle_y, float angle_z, float accel_x, float accel_y, float accel_z) { #if MODE_SYSTEMID_ENABLED == ENABLED struct log_SysIdD pkt_sidd = { LOG_PACKET_HEADER_INIT(LOG_SYSIDD_MSG), time_us : AP_HAL::micros64(), waveform_time : waveform_time, waveform_sample : waveform_sample, waveform_freq : waveform_freq, angle_x : angle_x, angle_y : angle_y, angle_z : angle_z, accel_x : accel_x, accel_y : accel_y, accel_z : accel_z }; logger.WriteBlock(&pkt_sidd, sizeof(pkt_sidd)); #endif } struct PACKED log_SysIdS { LOG_PACKET_HEADER; uint64_t time_us; uint8_t systemID_axis; float waveform_magnitude; float frequency_start; float frequency_stop; float time_fade_in; float time_const_freq; float time_record; float time_fade_out; }; // Write an rate packet void Copter::Log_Write_SysID_Setup(uint8_t systemID_axis, float waveform_magnitude, float frequency_start, float frequency_stop, float time_fade_in, float time_const_freq, float time_record, float time_fade_out) { #if MODE_SYSTEMID_ENABLED == ENABLED struct log_SysIdS pkt_sids = { LOG_PACKET_HEADER_INIT(LOG_SYSIDS_MSG), time_us : AP_HAL::micros64(), systemID_axis : systemID_axis, waveform_magnitude : waveform_magnitude, frequency_start : frequency_start, frequency_stop : frequency_stop, time_fade_in : time_fade_in, time_const_freq : time_const_freq, time_record : time_record, time_fade_out : time_fade_out }; logger.WriteBlock(&pkt_sids, sizeof(pkt_sids)); #endif } #if FRAME_CONFIG == HELI_FRAME struct PACKED log_Heli { LOG_PACKET_HEADER; uint64_t time_us; float desired_rotor_speed; float main_rotor_speed; float governor_output; float control_output; }; // Write an helicopter packet void Copter::Log_Write_Heli() { struct log_Heli pkt_heli = { LOG_PACKET_HEADER_INIT(LOG_HELI_MSG), time_us : AP_HAL::micros64(), desired_rotor_speed : motors->get_desired_rotor_speed(), main_rotor_speed : motors->get_main_rotor_speed(), governor_output : motors->get_governor_output(), control_output : motors->get_control_output(), }; logger.WriteBlock(&pkt_heli, sizeof(pkt_heli)); } #endif // precision landing logging struct PACKED log_Precland { LOG_PACKET_HEADER; uint64_t time_us; uint8_t healthy; uint8_t target_acquired; float pos_x; float pos_y; float vel_x; float vel_y; float meas_x; float meas_y; float meas_z; uint32_t last_meas; uint32_t ekf_outcount; uint8_t estimator; }; // Write a precision landing entry void Copter::Log_Write_Precland() { #if PRECISION_LANDING == ENABLED // exit immediately if not enabled if (!precland.enabled()) { return; } Vector3f target_pos_meas = Vector3f(0.0f,0.0f,0.0f); Vector2f target_pos_rel = Vector2f(0.0f,0.0f); Vector2f target_vel_rel = Vector2f(0.0f,0.0f); precland.get_target_position_relative_cm(target_pos_rel); precland.get_target_velocity_relative_cms(target_vel_rel); precland.get_target_position_measurement_cm(target_pos_meas); struct log_Precland pkt = { LOG_PACKET_HEADER_INIT(LOG_PRECLAND_MSG), time_us : AP_HAL::micros64(), healthy : precland.healthy(), target_acquired : precland.target_acquired(), pos_x : target_pos_rel.x, pos_y : target_pos_rel.y, vel_x : target_vel_rel.x, vel_y : target_vel_rel.y, meas_x : target_pos_meas.x, meas_y : target_pos_meas.y, meas_z : target_pos_meas.z, last_meas : precland.last_backend_los_meas_ms(), ekf_outcount : precland.ekf_outlier_count(), estimator : precland.estimator_type() }; logger.WriteBlock(&pkt, sizeof(pkt)); #endif // PRECISION_LANDING == ENABLED } // guided target logging struct PACKED log_GuidedTarget { LOG_PACKET_HEADER; uint64_t time_us; uint8_t type; float pos_target_x; float pos_target_y; float pos_target_z; float vel_target_x; float vel_target_y; float vel_target_z; }; // Write a Guided mode target // pos_target is lat, lon, alt OR offset from ekf origin in cm OR roll, pitch, yaw target in centi-degrees // vel_target is cm/s void Copter::Log_Write_GuidedTarget(uint8_t target_type, const Vector3f& pos_target, const Vector3f& vel_target) { struct log_GuidedTarget pkt = { LOG_PACKET_HEADER_INIT(LOG_GUIDEDTARGET_MSG), time_us : AP_HAL::micros64(), type : target_type, pos_target_x : pos_target.x, pos_target_y : pos_target.y, pos_target_z : pos_target.z, vel_target_x : vel_target.x, vel_target_y : vel_target.y, vel_target_z : vel_target.z }; logger.WriteBlock(&pkt, sizeof(pkt)); } // type and unit information can be found in // libraries/AP_Logger/Logstructure.h; search for "log_Units" for // units and "Format characters" for field type information const struct LogStructure Copter::log_structure[] = { LOG_COMMON_STRUCTURES, // @LoggerMessage: PTUN // @Description: Parameter Tuning information // @URL: https://ardupilot.org/copter/docs/tuning.html#in-flight-tuning // @Field: TimeUS: Time since system startup // @Field: Param: Parameter being tuned // @Field: TunVal: Normalized value used inside tuning() function // @Field: TunMin: Tuning minimum limit // @Field: TunMax: Tuning maximum limit { LOG_PARAMTUNE_MSG, sizeof(log_ParameterTuning), "PTUN", "QBfff", "TimeUS,Param,TunVal,TunMin,TunMax", "s----", "F----" }, // @LoggerMessage: CTUN // @Description: Control Tuning information // @Field: TimeUS: Time since system startup // @Field: ThI: throttle input // @Field: ABst: angle boost // @Field: ThO: throttle output // @Field: ThH: calculated hover throttle // @Field: DAlt: desired altitude // @Field: Alt: achieved altitude // @Field: BAlt: barometric altitude // @Field: DSAlt: desired rangefinder altitude // @Field: SAlt: achieved rangefinder altitude // @Field: TAlt: terrain altitude // @Field: DCRt: desired climb rate // @Field: CRt: climb rate // @LoggerMessage: D16 // @Description: Generic 16-bit-signed-integer storage // @Field: TimeUS: Time since system startup // @Field: Id: Data type identifier // @Field: Value: Value // @LoggerMessage: DU16 // @Description: Generic 16-bit-unsigned-integer storage // @Field: TimeUS: Time since system startup // @Field: Id: Data type identifier // @Field: Value: Value // @LoggerMessage: D32 // @Description: Generic 32-bit-signed-integer storage // @Field: TimeUS: Time since system startup // @Field: Id: Data type identifier // @Field: Value: Value // @LoggerMessage: DFLT // @Description: Generic float storage // @Field: TimeUS: Time since system startup // @Field: Id: Data type identifier // @Field: Value: Value // @LoggerMessage: DU32 // @Description: Generic 32-bit-unsigned-integer storage // @Field: TimeUS: Time since system startup // @Field: Id: Data type identifier // @Field: Value: Value { LOG_CONTROL_TUNING_MSG, sizeof(log_Control_Tuning), "CTUN", "Qffffffefffhh", "TimeUS,ThI,ABst,ThO,ThH,DAlt,Alt,BAlt,DSAlt,SAlt,TAlt,DCRt,CRt", "s----mmmmmmnn", "F----00B000BB" }, // @LoggerMessage: MOTB // @Description: Battery information // @Field: TimeUS: Time since system startup // @Field: LiftMax: Maximum motor compensation gain // @Field: BatVolt: Ratio betwen detected battery voltage and maximum battery voltage // @Field: BatRes: Estimated battery resistance // @Field: ThLimit: Throttle limit set due to battery current limitations { LOG_MOTBATT_MSG, sizeof(log_MotBatt), "MOTB", "Qffff", "TimeUS,LiftMax,BatVolt,BatRes,ThLimit", "s-vw-", "F-00-" }, { LOG_DATA_INT16_MSG, sizeof(log_Data_Int16t), "D16", "QBh", "TimeUS,Id,Value", "s--", "F--" }, { LOG_DATA_UINT16_MSG, sizeof(log_Data_UInt16t), "DU16", "QBH", "TimeUS,Id,Value", "s--", "F--" }, { LOG_DATA_INT32_MSG, sizeof(log_Data_Int32t), "D32", "QBi", "TimeUS,Id,Value", "s--", "F--" }, { LOG_DATA_UINT32_MSG, sizeof(log_Data_UInt32t), "DU32", "QBI", "TimeUS,Id,Value", "s--", "F--" }, { LOG_DATA_FLOAT_MSG, sizeof(log_Data_Float), "DFLT", "QBf", "TimeUS,Id,Value", "s--", "F--" }, // @LoggerMessage: HELI // @Description: Helicopter related messages // @Field: TimeUS: Time since system startup // @Field: DRRPM: Desired rotor speed // @Field: ERRPM: Estimated rotor speed // @Field: Gov: Governor Output // @Field: Throt: Throttle output #if FRAME_CONFIG == HELI_FRAME { LOG_HELI_MSG, sizeof(log_Heli), "HELI", "Qffff", "TimeUS,DRRPM,ERRPM,Gov,Throt", "s----", "F----" }, #endif // @LoggerMessage: PL // @Description: Precision Landing messages // @Field: TimeUS: Time since system startup // @Field: Heal: True if Precision Landing is healthy // @Field: TAcq: True if landing target is detected // @Field: pX: Target position relative to vehicle, X-Axis (0 if target not found) // @Field: pY: Target position relative to vehicle, Y-Axis (0 if target not found) // @Field: vX: Target velocity relative to vehicle, X-Axis (0 if target not found) // @Field: vY: Target velocity relative to vehicle, Y-Axis (0 if target not found) // @Field: mX: Target's relative to origin position as 3-D Vector, X-Axis // @Field: mY: Target's relative to origin position as 3-D Vector, Y-Axis // @Field: mZ: Target's relative to origin position as 3-D Vector, Z-Axis // @Field: LastMeasMS: Time when target was last detected // @Field: EKFOutl: EKF's outlier count // @Field: Est: Type of estimator used #if PRECISION_LANDING == ENABLED { LOG_PRECLAND_MSG, sizeof(log_Precland), "PL", "QBBfffffffIIB", "TimeUS,Heal,TAcq,pX,pY,vX,vY,mX,mY,mZ,LastMeasMS,EKFOutl,Est", "s--mmnnmmms--","F--BBBBBBBC--" }, #endif // @LoggerMessage: SIDD // @Description: System ID data // @Field: TimeUS: Time since system startup // @Field: Time: Time reference for waveform // @Field: Targ: Current waveform sample // @Field: F: Instantaneous waveform frequency // @Field: Gx: Delta angle, X-Axis // @Field: Gy: Delta angle, Y-Axis // @Field: Gz: Delta angle, Z-Axis // @Field: Ax: Delta velocity, X-Axis // @Field: Ay: Delta velocity, Y-Axis // @Field: Az: Delta velocity, Z-Axis { LOG_SYSIDD_MSG, sizeof(log_SysIdD), "SIDD", "Qfffffffff", "TimeUS,Time,Targ,F,Gx,Gy,Gz,Ax,Ay,Az", "ss-zkkkooo", "F---------" }, // @LoggerMessage: SIDS // @Description: System ID settings // @Field: TimeUS: Time since system startup // @Field: Ax: The axis which is being excited // @Field: Mag: Magnitude of the chirp waveform // @Field: FSt: Frequency at the start of chirp // @Field: FSp: Frequency at the end of chirp // @Field: TFin: Time to reach maximum amplitude of chirp // @Field: TC: Time at constant frequency before chirp starts // @Field: TR: Time taken to complete chirp waveform // @Field: TFout: Time to reach zero amplitude after chirp finishes { LOG_SYSIDS_MSG, sizeof(log_SysIdS), "SIDS", "QBfffffff", "TimeUS,Ax,Mag,FSt,FSp,TFin,TC,TR,TFout", "s--ssssss", "F--------" }, // @LoggerMessage: GUID // @Description: Guided mode target information // @Field: TimeUS: Time since system startup // @Field: Type: Type of guided mode // @Field: pX: Target position, X-Axis // @Field: pY: Target position, Y-Axis // @Field: pZ: Target position, Z-Axis // @Field: vX: Target velocity, X-Axis // @Field: vY: Target velocity, Y-Axis // @Field: vZ: Target velocity, Z-Axis { LOG_GUIDEDTARGET_MSG, sizeof(log_GuidedTarget), "GUID", "QBffffff", "TimeUS,Type,pX,pY,pZ,vX,vY,vZ", "s-mmmnnn", "F-BBBBBB" }, }; void Copter::Log_Write_Vehicle_Startup_Messages() { // only 200(?) bytes are guaranteed by AP_Logger logger.Write_MessageF("Frame: %s", get_frame_string()); logger.Write_Mode((uint8_t)control_mode, control_mode_reason); ahrs.Log_Write_Home_And_Origin(); gps.Write_AP_Logger_Log_Startup_messages(); } void Copter::log_init(void) { logger.Init(log_structure, ARRAY_SIZE(log_structure)); } #else // LOGGING_ENABLED void Copter::Log_Write_Control_Tuning() {} void Copter::Log_Write_Performance() {} void Copter::Log_Write_Attitude(void) {} void Copter::Log_Write_EKF_POS() {} void Copter::Log_Write_MotBatt() {} void Copter::Log_Write_Data(LogDataID id, int32_t value) {} void Copter::Log_Write_Data(LogDataID id, uint32_t value) {} void Copter::Log_Write_Data(LogDataID id, int16_t value) {} void Copter::Log_Write_Data(LogDataID id, uint16_t value) {} void Copter::Log_Write_Data(LogDataID id, float value) {} void Copter::Log_Write_Parameter_Tuning(uint8_t param, float tuning_val, float tune_min, float tune_max) {} void Copter::Log_Sensor_Health() {} void Copter::Log_Write_Precland() {} void Copter::Log_Write_GuidedTarget(uint8_t target_type, const Vector3f& pos_target, const Vector3f& vel_target) {} void Copter::Log_Write_SysID_Setup(uint8_t systemID_axis, float waveform_magnitude, float frequency_start, float frequency_stop, float time_fade_in, float time_const_freq, float time_record, float time_fade_out) {} void Copter::Log_Write_SysID_Data(float waveform_time, float waveform_sample, float waveform_freq, float angle_x, float angle_y, float angle_z, float accel_x, float accel_y, float accel_z) {} void Copter::Log_Write_Vehicle_Startup_Messages() {} #if FRAME_CONFIG == HELI_FRAME void Copter::Log_Write_Heli() {} #endif void Copter::log_init(void) {} #endif // LOGGING_ENABLED