mirror of https://github.com/ArduPilot/ardupilot
163 lines
6.0 KiB
C++
163 lines
6.0 KiB
C++
#pragma once
|
|
|
|
#include <GCS_MAVLink/GCS_MAVLink.h>
|
|
|
|
class DataFlash_Class;
|
|
|
|
namespace SITL {
|
|
|
|
struct sitl_fdm {
|
|
// this is the structure passed between FDM models and the main SITL code
|
|
uint64_t timestamp_us;
|
|
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
|
|
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
|
|
};
|
|
|
|
// 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);
|
|
}
|
|
|
|
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[];
|
|
|
|
// 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; // pitot tube failure
|
|
AP_Float gps_noise; // amplitude of the gps altitude error
|
|
|
|
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_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 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_Int8 pin_mask; // for GPIO emulation
|
|
AP_Float speedup; // simulation speedup
|
|
|
|
// wind control
|
|
float wind_speed_active;
|
|
float wind_direction_active;
|
|
AP_Float wind_speed;
|
|
AP_Float wind_direction;
|
|
AP_Float wind_turbulance;
|
|
AP_Float gps_drift_alt;
|
|
|
|
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)
|
|
|
|
uint16_t irlock_port;
|
|
|
|
void simstate_send(mavlink_channel_t chan);
|
|
|
|
void Log_Write_SIMSTATE(DataFlash_Class *dataflash);
|
|
|
|
// 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);
|
|
};
|
|
|
|
} // namespace SITL
|