#pragma once #include #include #include #include "SIM_Sprayer.h" #include "SIM_Gripper_Servo.h" #include "SIM_Gripper_EPM.h" #include "SIM_Parachute.h" #include "SIM_Precland.h" namespace SITL { struct vector3f_array { uint16_t length; Vector3f *data; }; struct float_array { uint16_t length; float *data; }; struct sitl_fdm { // this is the structure passed between FDM models and the main SITL code uint64_t timestamp_us; Location home; double latitude, longitude; // degrees double altitude; // MSL double heading; // degrees double speedN, speedE, speedD; // m/s double xAccel, yAccel, zAccel; // m/s/s in body frame double rollRate, pitchRate, yawRate; // degrees/s/s in body frame double rollDeg, pitchDeg, yawDeg; // euler angles, degrees Quaternion quaternion; double airspeed; // m/s double battery_voltage; // Volts double battery_current; // Amps double rpm1; // main prop RPM double rpm2; // secondary RPM uint8_t rcin_chan_count; float rcin[8]; // RC input 0..1 double range; // rangefinder value Vector3f bodyMagField; // Truth XYZ magnetic field vector in body-frame. Includes motor interference. Units are milli-Gauss. Vector3f angAccel; // Angular acceleration in degrees/s/s about the XYZ body axes struct { // data from simulated laser scanner, if available struct vector3f_array points; struct float_array ranges; } scanner; }; // number of rc output channels #define SITL_NUM_CHANNELS 16 class SITL { public: SITL() { // set a default compass offset mag_ofs.set(Vector3f(5, 13, -18)); AP_Param::setup_object_defaults(this, var_info); AP_Param::setup_object_defaults(this, var_info2); if (_singleton != nullptr) { AP_HAL::panic("Too many SITL instances"); } _singleton = this; } /* Do not allow copies */ SITL(const SITL &other) = delete; SITL &operator=(const SITL&) = delete; static SITL *_singleton; static SITL *get_singleton() { return _singleton; } enum SITL_RCFail { SITL_RCFail_None = 0, SITL_RCFail_NoPulses = 1, SITL_RCFail_Throttle950 = 2, }; enum GPSType { GPS_TYPE_NONE = 0, GPS_TYPE_UBLOX = 1, GPS_TYPE_MTK = 2, GPS_TYPE_MTK16 = 3, GPS_TYPE_MTK19 = 4, GPS_TYPE_NMEA = 5, GPS_TYPE_SBP = 6, GPS_TYPE_FILE = 7, GPS_TYPE_NOVA = 8, GPS_TYPE_SBP2 = 9, }; struct sitl_fdm state; // loop update rate in Hz uint16_t update_rate_hz; // true when motors are active bool motors_on; // height above ground float height_agl; static const struct AP_Param::GroupInfo var_info[]; static const struct AP_Param::GroupInfo var_info2[]; // noise levels for simulated sensors AP_Float baro_noise; // in metres AP_Float baro_drift; // in metres per second AP_Float baro_glitch; // glitch in meters AP_Float gyro_noise; // in degrees/second AP_Vector3f gyro_scale; // percentage AP_Float accel_noise; // in m/s/s AP_Float accel2_noise; // in m/s/s AP_Vector3f accel_bias; // in m/s/s AP_Vector3f accel2_bias; // in m/s/s AP_Float arspd_noise; // in m/s AP_Float arspd_fail; // 1st pitot tube failure AP_Float arspd2_fail; // 2nd pitot tube failure AP_Float arspd_fail_pressure; // 1st pitot tube failure pressure AP_Float arspd_fail_pitot_pressure; // 1st pitot tube failure pressure AP_Float arspd2_fail_pressure; // 2nd pitot tube failure pressure AP_Float arspd2_fail_pitot_pressure; // 2nd pitot tube failure pressure AP_Float gps_noise; // amplitude of the gps altitude error AP_Int16 gps_lock_time; // delay in seconds before GPS gets lock AP_Int16 gps_alt_offset; // gps alt error AP_Int8 vicon_observation_history_length; // frame delay for vicon messages AP_Float mag_noise; // in mag units (earth field is 818) AP_Float mag_error; // in degrees AP_Vector3f mag_mot; // in mag units per amp AP_Vector3f mag_ofs; // in mag units AP_Vector3f mag_diag; // diagonal corrections AP_Vector3f mag_offdiag; // off-diagonal corrections AP_Int8 mag_orient; // external compass orientation AP_Float servo_speed; // servo speed in seconds AP_Float sonar_glitch;// probablility between 0-1 that any given sonar sample will read as max distance AP_Float sonar_noise; // in metres AP_Float sonar_scale; // meters per volt AP_Float drift_speed; // degrees/second/minute AP_Float drift_time; // period in minutes AP_Float engine_mul; // engine multiplier AP_Int8 engine_fail; // engine servo to fail (0-7) AP_Int8 gps_disable; // disable simulated GPS AP_Int8 gps2_enable; // enable 2nd simulated GPS AP_Int8 gps_delay; // delay in samples AP_Int8 gps_type; // see enum GPSType AP_Int8 gps2_type; // see enum GPSType AP_Float gps_byteloss;// byte loss as a percent AP_Int8 gps_numsats; // number of visible satellites AP_Vector3f gps_glitch; // glitch offsets in lat, lon and altitude AP_Vector3f gps2_glitch; // glitch offsets in lat, lon and altitude for 2nd GPS AP_Int8 gps_hertz; // GPS update rate in Hz AP_Float batt_voltage; // battery voltage base AP_Float accel_fail; // accelerometer failure value AP_Int8 rc_fail; // fail RC input AP_Int8 rc_chancount; // channel count AP_Int8 baro_disable; // disable simulated barometer AP_Int8 float_exception; // enable floating point exception checks AP_Int8 flow_enable; // enable simulated optflow AP_Int16 flow_rate; // optflow data rate (Hz) AP_Int8 flow_delay; // optflow data delay AP_Int8 terrain_enable; // enable using terrain for height AP_Int16 pin_mask; // for GPIO emulation AP_Float speedup; // simulation speedup AP_Int8 odom_enable; // enable visual odomotry data AP_Int8 telem_baudlimit_enable; // enable baudrate limiting on links AP_Float flow_noise; // optical flow measurement noise (rad/sec) AP_Int8 baro_count; // number of simulated baros to create AP_Int8 gps_hdg_enabled; // enable the output of a NMEA heading HDT sentence AP_Int32 loop_delay; // extra delay to add to every loop // wind control enum WindType { WIND_TYPE_SQRT = 0, WIND_TYPE_NO_LIMIT = 1, WIND_TYPE_COEF = 2, }; float wind_speed_active; float wind_direction_active; float wind_dir_z_active; AP_Float wind_speed; AP_Float wind_direction; AP_Float wind_turbulance; AP_Float gps_drift_alt; AP_Float wind_dir_z; AP_Int8 wind_type; // enum WindLimitType AP_Float wind_type_alt; AP_Float wind_type_coef; AP_Int16 baro_delay; // barometer data delay in ms AP_Int16 mag_delay; // magnetometer data delay in ms AP_Int16 wind_delay; // windspeed data delay in ms // ADSB related run-time options AP_Int16 adsb_plane_count; AP_Float adsb_radius_m; AP_Float adsb_altitude_m; AP_Int8 adsb_tx; // Earth magnetic field anomaly AP_Vector3f mag_anomaly_ned; // NED anomaly vector at ground level (mGauss) AP_Float mag_anomaly_hgt; // height above ground where anomally strength has decayed to 1/8 of the ground level value (m) // Body frame sensor position offsets AP_Vector3f imu_pos_offset; // XYZ position of the IMU accelerometer relative to the body frame origin (m) AP_Vector3f gps_pos_offset; // XYZ position of the GPS antenna phase centre relative to the body frame origin (m) AP_Vector3f rngfnd_pos_offset; // XYZ position of the range finder zero range datum relative to the body frame origin (m) AP_Vector3f optflow_pos_offset; // XYZ position of the optical flow sensor focal point relative to the body frame origin (m) // temperature control AP_Float temp_start; AP_Float temp_flight; AP_Float temp_tconst; AP_Float temp_baro_factor; // differential pressure sensor tube order AP_Int8 arspd_signflip; // weight on wheels pin AP_Int8 wow_pin; // vibration frequencies in Hz on each axis AP_Vector3f vibe_freq; // gyro and accel fail masks AP_Int8 gyro_fail_mask; AP_Int8 accel_fail_mask; struct { AP_Float x; AP_Float y; AP_Float z; AP_Int32 t; uint32_t start_ms; } shove; struct { AP_Float x; AP_Float y; AP_Float z; AP_Int32 t; uint32_t start_ms; } twist; AP_Int8 gnd_behav; struct { AP_Int8 enable; // 0: disabled, 1: roll and pitch, 2: roll, pitch and heave AP_Float length; // m AP_Float amp; // m AP_Float direction; // deg (direction wave is coming from) AP_Float speed; // m/s } wave; struct { AP_Float direction; // deg (direction tide is coming from) AP_Float speed; // m/s } tide; // original simulated position struct { AP_Float lat; AP_Float lng; AP_Float alt; // metres AP_Float hdg; // 0 to 360 } opos; uint16_t irlock_port; void simstate_send(mavlink_channel_t chan); void Log_Write_SIMSTATE(); // convert a set of roll rates from earth frame to body frame static void convert_body_frame(double rollDeg, double pitchDeg, double rollRate, double pitchRate, double yawRate, double *p, double *q, double *r); // convert a set of roll rates from body frame to earth frame static Vector3f convert_earth_frame(const Matrix3f &dcm, const Vector3f &gyro); Sprayer sprayer_sim; Gripper_Servo gripper_sim; Gripper_EPM gripper_epm_sim; Parachute parachute_sim; SIM_Precland precland_sim; }; } // namespace SITL namespace AP { SITL::SITL *sitl(); };