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115 lines
4.0 KiB
115 lines
4.0 KiB
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- |
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#ifndef __SITL_H__ |
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#define __SITL_H__ |
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#include <AP_Param.h> |
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#include <AP_Common.h> |
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#include <AP_Math.h> |
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#include <GCS_MAVLink.h> |
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#include <DataFlash.h> |
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struct PACKED sitl_fdm { |
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// this is the packet sent by the simulator |
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// to the APM executable to update the simulator state |
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// All values are little-endian |
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uint64_t timestamp_us; |
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double latitude, longitude; // degrees |
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double altitude; // MSL |
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double heading; // degrees |
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double speedN, speedE, speedD; // m/s |
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double xAccel, yAccel, zAccel; // m/s/s in body frame |
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double rollRate, pitchRate, yawRate; // degrees/s/s in body frame |
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double rollDeg, pitchDeg, yawDeg; // euler angles, degrees |
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double airspeed; // m/s |
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uint32_t magic; // 0x4c56414f |
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}; |
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class SITL |
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{ |
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public: |
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SITL() { |
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// set a default compass offset |
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mag_ofs.set(Vector3f(5, 13, -18)); |
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AP_Param::setup_object_defaults(this, var_info); |
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} |
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enum GPSType { |
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GPS_TYPE_NONE = 0, |
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GPS_TYPE_UBLOX = 1, |
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GPS_TYPE_MTK = 2, |
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GPS_TYPE_MTK16 = 3, |
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GPS_TYPE_MTK19 = 4, |
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GPS_TYPE_NMEA = 5, |
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GPS_TYPE_SBP = 6, |
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}; |
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struct sitl_fdm state; |
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static const struct AP_Param::GroupInfo var_info[]; |
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// noise levels for simulated sensors |
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AP_Float baro_noise; // in metres |
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AP_Float baro_drift; // in metres per second |
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AP_Float baro_glitch; // glitch in meters |
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AP_Float gyro_noise; // in degrees/second |
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AP_Float accel_noise; // in m/s/s |
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AP_Vector3f accel_bias; // in m/s/s |
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AP_Float aspd_noise; // in m/s |
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AP_Float mag_noise; // in mag units (earth field is 818) |
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AP_Float mag_error; // in degrees |
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AP_Vector3f mag_mot; // in mag units per amp |
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AP_Vector3f mag_ofs; // in mag units |
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AP_Float servo_rate; // servo speed in degrees/second |
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AP_Float sonar_glitch;// probablility between 0-1 that any given sonar sample will read as max distance |
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AP_Float sonar_noise; // in metres |
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AP_Float sonar_scale; // meters per volt |
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AP_Float drift_speed; // degrees/second/minute |
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AP_Float drift_time; // period in minutes |
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AP_Float engine_mul; // engine multiplier |
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AP_Int8 gps_disable; // disable simulated GPS |
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AP_Int8 gps2_enable; // enable 2nd simulated GPS |
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AP_Int8 gps_delay; // delay in samples |
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AP_Int8 gps_type; // see enum GPSType |
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AP_Float gps_byteloss;// byte loss as a percent |
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AP_Int8 gps_numsats; // number of visible satellites |
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AP_Vector3f gps_glitch; // glitch offsets in lat, lon and altitude |
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AP_Int8 gps_hertz; // GPS update rate in Hz |
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AP_Float batt_voltage; // battery voltage base |
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AP_Float accel_fail; // accelerometer failure value |
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AP_Int8 rc_fail; // fail RC input |
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AP_Int8 baro_disable; // disable simulated barometer |
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AP_Int8 float_exception; // enable floating point exception checks |
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AP_Int8 flow_enable; // enable simulated optflow |
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AP_Int16 flow_rate; // optflow data rate (Hz) |
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AP_Int8 flow_delay; // optflow data delay |
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AP_Int8 terrain_enable; // enable using terrain for height |
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// wind control |
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AP_Float wind_speed; |
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AP_Float wind_direction; |
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AP_Float wind_turbulance; |
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AP_Float gps_drift_alt; |
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AP_Int16 baro_delay; // barometer data delay in ms |
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AP_Int16 mag_delay; // magnetometer data delay in ms |
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AP_Int16 wind_delay; // windspeed data delay in ms |
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void simstate_send(mavlink_channel_t chan); |
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void Log_Write_SIMSTATE(DataFlash_Class &dataflash); |
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// convert a set of roll rates from earth frame to body frame |
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static void convert_body_frame(double rollDeg, double pitchDeg, |
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double rollRate, double pitchRate, double yawRate, |
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double *p, double *q, double *r); |
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// convert a set of roll rates from body frame to earth frame |
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static Vector3f convert_earth_frame(const Matrix3f &dcm, const Vector3f &gyro); |
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}; |
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#endif // __SITL_H__
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