Paparazzi UAS
v7.0_unstable
Paparazzi is a free software Unmanned Aircraft System.
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Multiplicative Extended Kalman Filter in rotation matrix formulation. More...
Go to the source code of this file.
Data Structures | |
struct | MekfWindState |
filter state vector More... | |
struct | MekfWindInputs |
filter command vector More... | |
struct | MekfWindMeasurements |
filter measurement vector More... | |
struct | InsMekfWindPrivate |
private filter structure More... | |
Macros | |
#define | eigen_assert(_cond) { if (!(_cond)) { while(1) ; } } |
#define | INS_MEKF_WIND_P0_QUAT 0.007615f |
#define | INS_MEKF_WIND_P0_SPEED 1.E+2f |
#define | INS_MEKF_WIND_P0_POS 1.E+1f |
#define | INS_MEKF_WIND_P0_RATES_BIAS 1.E-3f |
#define | INS_MEKF_WIND_P0_ACCEL_BIAS 1.E-3f |
#define | INS_MEKF_WIND_P0_BARO_BIAS 1.E-3f |
#define | INS_MEKF_WIND_P0_WIND 1.E-0f |
#define | INS_MEKF_WIND_Q_GYRO 1.E-2f |
#define | INS_MEKF_WIND_Q_ACCEL 1.E-2f |
#define | INS_MEKF_WIND_Q_RATES_BIAS 1.E-6f |
#define | INS_MEKF_WIND_Q_ACCEL_BIAS 1.E-6f |
#define | INS_MEKF_WIND_Q_BARO_BIAS 1.E-3f |
#define | INS_MEKF_WIND_Q_WIND 1.E+1f |
#define | INS_MEKF_WIND_R_SPEED 0.1f |
#define | INS_MEKF_WIND_R_SPEED_Z 0.2f |
#define | INS_MEKF_WIND_R_POS 2.0f |
#define | INS_MEKF_WIND_R_POS_Z 4.0f |
#define | INS_MEKF_WIND_R_MAG 1.f |
#define | INS_MEKF_WIND_R_BARO 2.f |
#define | INS_MEKF_WIND_R_AIRSPEED 0.1f |
#define | INS_MEKF_WIND_R_AOA 0.1f |
#define | INS_MEKF_WIND_R_AOS 0.1f |
#define | INS_MEKF_WIND_DISABLE_WIND true |
#define | mwp mekf_wind_private |
Typedefs | |
typedef Matrix< float, MEKF_WIND_COV_SIZE, MEKF_WIND_COV_SIZE > | MEKFWCov |
typedef Matrix< float, MEKF_WIND_PROC_NOISE_SIZE, MEKF_WIND_PROC_NOISE_SIZE > | MEKFWPNoise |
typedef Matrix< float, MEKF_WIND_MEAS_NOISE_SIZE, MEKF_WIND_MEAS_NOISE_SIZE > | MEKFWMNoise |
Functions | |
static const Vector3f | gravity (0.f, 0.f, 9.81f) |
static void | init_mekf_state (void) |
static Quaternionf | quat_add (const Quaternionf &q1, const Quaternionf &q2) |
static Quaternionf | quat_smul (const Quaternionf &q1, float scal) |
static Matrix3f | skew_sym (const Vector3f &v) |
build skew symetric matrix from vector m = [ 0, -v(2), v(1) ] [ v(2), 0, -v(0) ] [ -v(1), v(0), 0 ] More... | |
void | ins_mekf_wind_init (void) |
Init function. More... | |
void | ins_mekf_wind_set_mag_h (const struct FloatVect3 *mag_h) |
void | ins_mekf_wind_reset (void) |
void | ins_mekf_wind_propagate (struct FloatRates *gyro, struct FloatVect3 *acc, float dt) |
Full INS propagation. More... | |
void | ins_mekf_wind_propagate_ahrs (struct FloatRates *gyro, struct FloatVect3 *acc, float dt) |
AHRS-only propagation + accel correction. More... | |
void | ins_mekf_wind_align (struct FloatRates *gyro_bias, struct FloatQuat *quat) |
void | ins_mekf_wind_update_mag (struct FloatVect3 *mag, bool attitude_only) |
void | ins_mekf_wind_update_baro (float baro_alt) |
void | ins_mekf_wind_update_pos_speed (struct FloatVect3 *pos, struct FloatVect3 *speed) |
void | ins_mekf_wind_update_airspeed (float airspeed) |
void | ins_mekf_wind_update_incidence (float aoa, float aos) |
struct NedCoor_f | ins_mekf_wind_get_pos_ned (void) |
Getter/Setter functions. More... | |
void | ins_mekf_wind_set_pos_ned (struct NedCoor_f *p) |
struct NedCoor_f | ins_mekf_wind_get_speed_ned (void) |
void | ins_mekf_wind_set_speed_ned (struct NedCoor_f *s) |
struct NedCoor_f | ins_mekf_wind_get_accel_ned (void) |
struct FloatQuat | ins_mekf_wind_get_quat (void) |
void | ins_mekf_wind_set_quat (struct FloatQuat *quat) |
struct FloatRates | ins_mekf_wind_get_body_rates (void) |
struct NedCoor_f | ins_mekf_wind_get_wind_ned (void) |
struct NedCoor_f | ins_mekf_wind_get_airspeed_body (void) |
float | ins_mekf_wind_get_airspeed_norm (void) |
struct FloatVect3 | ins_mekf_wind_get_accel_bias (void) |
struct FloatRates | ins_mekf_wind_get_rates_bias (void) |
float | ins_mekf_wind_get_baro_bias (void) |
void | ins_mekf_wind_update_params (void) |
Variables | |
struct ins_mekf_wind_parameters | ins_mekf_wind_params |
static struct InsMekfWindPrivate | mekf_wind_private |
Multiplicative Extended Kalman Filter in rotation matrix formulation.
Estimate attitude, ground speed, position, gyro bias, accelerometer bias and wind speed.
Using Eigen library
Definition in file ins_mekf_wind.cpp.
struct MekfWindState |
filter state vector
Definition at line 93 of file ins_mekf_wind.cpp.
Data Fields | ||
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Vector3f | accel | |
Vector3f | accel_bias | |
float | baro_bias | |
Vector3f | pos | |
Quaternionf | quat | |
Vector3f | rates_bias | |
Vector3f | speed | |
Vector3f | wind |
struct MekfWindInputs |
filter command vector
Definition at line 106 of file ins_mekf_wind.cpp.
Data Fields | ||
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Vector3f | accel | |
Vector3f | rates |
struct MekfWindMeasurements |
filter measurement vector
Definition at line 113 of file ins_mekf_wind.cpp.
Data Fields | ||
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float | airspeed | |
float | aoa | |
float | aos | |
float | baro_alt | |
Vector3f | mag | |
Vector3f | pos | |
Vector3f | speed |
struct InsMekfWindPrivate |
private filter structure
Definition at line 125 of file ins_mekf_wind.cpp.
Data Fields | ||
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struct MekfWindInputs | inputs | |
Vector3f | mag_h | |
struct MekfWindMeasurements | measurements | |
MEKFWCov | P | |
MEKFWPNoise | Q | |
MEKFWMNoise | R | |
struct MekfWindState | state |
#define eigen_assert | ( | _cond | ) | { if (!(_cond)) { while(1) ; } } |
Definition at line 38 of file ins_mekf_wind.cpp.
#define INS_MEKF_WIND_DISABLE_WIND true |
Definition at line 213 of file ins_mekf_wind.cpp.
Definition at line 153 of file ins_mekf_wind.cpp.
Definition at line 156 of file ins_mekf_wind.cpp.
Definition at line 147 of file ins_mekf_wind.cpp.
#define INS_MEKF_WIND_P0_QUAT 0.007615f |
Definition at line 141 of file ins_mekf_wind.cpp.
Definition at line 150 of file ins_mekf_wind.cpp.
Definition at line 144 of file ins_mekf_wind.cpp.
#define INS_MEKF_WIND_P0_WIND 1.E-0f |
Definition at line 159 of file ins_mekf_wind.cpp.
Definition at line 167 of file ins_mekf_wind.cpp.
Definition at line 173 of file ins_mekf_wind.cpp.
Definition at line 176 of file ins_mekf_wind.cpp.
Definition at line 164 of file ins_mekf_wind.cpp.
Definition at line 170 of file ins_mekf_wind.cpp.
Definition at line 179 of file ins_mekf_wind.cpp.
#define INS_MEKF_WIND_R_AIRSPEED 0.1f |
Definition at line 202 of file ins_mekf_wind.cpp.
#define INS_MEKF_WIND_R_AOA 0.1f |
Definition at line 205 of file ins_mekf_wind.cpp.
#define INS_MEKF_WIND_R_AOS 0.1f |
Definition at line 208 of file ins_mekf_wind.cpp.
#define INS_MEKF_WIND_R_BARO 2.f |
Definition at line 199 of file ins_mekf_wind.cpp.
#define INS_MEKF_WIND_R_MAG 1.f |
Definition at line 196 of file ins_mekf_wind.cpp.
#define INS_MEKF_WIND_R_POS 2.0f |
Definition at line 190 of file ins_mekf_wind.cpp.
#define INS_MEKF_WIND_R_POS_Z 4.0f |
Definition at line 193 of file ins_mekf_wind.cpp.
#define INS_MEKF_WIND_R_SPEED 0.1f |
Definition at line 184 of file ins_mekf_wind.cpp.
#define INS_MEKF_WIND_R_SPEED_Z 0.2f |
Definition at line 187 of file ins_mekf_wind.cpp.
#define mwp mekf_wind_private |
Definition at line 222 of file ins_mekf_wind.cpp.
typedef Matrix<float, MEKF_WIND_COV_SIZE, MEKF_WIND_COV_SIZE> MEKFWCov |
Definition at line 62 of file ins_mekf_wind.cpp.
typedef Matrix<float, MEKF_WIND_MEAS_NOISE_SIZE, MEKF_WIND_MEAS_NOISE_SIZE> MEKFWMNoise |
Definition at line 89 of file ins_mekf_wind.cpp.
typedef Matrix<float, MEKF_WIND_PROC_NOISE_SIZE, MEKF_WIND_PROC_NOISE_SIZE> MEKFWPNoise |
Definition at line 76 of file ins_mekf_wind.cpp.
enum MekfWindCovVar |
Covariance matrix elements and size.
Definition at line 51 of file ins_mekf_wind.cpp.
enum MekfWindMNoiseVar |
Measurement noise elements and size.
Definition at line 80 of file ins_mekf_wind.cpp.
enum MekfWindPNoiseVar |
Process noise elements and size.
Definition at line 66 of file ins_mekf_wind.cpp.
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Referenced by ins_mekf_wind_propagate(), and ins_mekf_wind_propagate_ahrs().
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Definition at line 229 of file ins_mekf_wind.cpp.
References MekfWindInputs::accel, MekfWindState::accel_bias, MekfWindMeasurements::airspeed, MekfWindMeasurements::aoa, MekfWindMeasurements::aos, MekfWindMeasurements::baro_alt, MekfWindState::baro_bias, InsMekfWindPrivate::inputs, INS_MEKF_WIND_P0_ACCEL_BIAS, INS_MEKF_WIND_P0_BARO_BIAS, INS_MEKF_WIND_P0_POS, INS_MEKF_WIND_P0_QUAT, INS_MEKF_WIND_P0_RATES_BIAS, INS_MEKF_WIND_P0_SPEED, INS_MEKF_WIND_P0_WIND, ins_mekf_wind_update_params(), MekfWindMeasurements::mag, InsMekfWindPrivate::measurements, MEKF_WIND_abx, MEKF_WIND_aby, MEKF_WIND_abz, MEKF_WIND_bb, mekf_wind_private, MEKF_WIND_px, MEKF_WIND_py, MEKF_WIND_pz, MEKF_WIND_qx, MEKF_WIND_qy, MEKF_WIND_qz, MEKF_WIND_rbp, MEKF_WIND_rbq, MEKF_WIND_rbr, MEKF_WIND_vx, MEKF_WIND_vy, MEKF_WIND_vz, MEKF_WIND_wx, MEKF_WIND_wy, MEKF_WIND_wz, InsMekfWindPrivate::P, MekfWindState::pos, MekfWindMeasurements::pos, MekfWindState::quat, MekfWindInputs::rates, MekfWindState::rates_bias, MekfWindState::speed, MekfWindMeasurements::speed, InsMekfWindPrivate::state, and MekfWindState::wind.
Referenced by ins_mekf_wind_init(), and ins_mekf_wind_reset().
void ins_mekf_wind_align | ( | struct FloatRates * | gyro_bias, |
struct FloatQuat * | quat | ||
) |
Definition at line 487 of file ins_mekf_wind.cpp.
References mwp, FloatRates::p, FloatRates::q, FloatQuat::qi, FloatQuat::qx, FloatQuat::qy, FloatQuat::qz, and FloatRates::r.
Referenced by aligner_cb().
struct FloatVect3 ins_mekf_wind_get_accel_bias | ( | void | ) |
Definition at line 816 of file ins_mekf_wind.cpp.
References mwp.
Referenced by gyro_cb(), and send_inv_filter().
struct NedCoor_f ins_mekf_wind_get_accel_ned | ( | void | ) |
Definition at line 748 of file ins_mekf_wind.cpp.
Referenced by gyro_cb(), and set_state_from_ins().
struct NedCoor_f ins_mekf_wind_get_airspeed_body | ( | void | ) |
Definition at line 776 of file ins_mekf_wind.cpp.
References mwp, FloatQuat::qi, FloatQuat::qx, FloatQuat::qy, and FloatQuat::qz.
float ins_mekf_wind_get_airspeed_norm | ( | void | ) |
Definition at line 816 of file ins_mekf_wind.cpp.
Referenced by gyro_cb(), send_inv_filter(), and send_wind().
float ins_mekf_wind_get_baro_bias | ( | void | ) |
Definition at line 841 of file ins_mekf_wind.cpp.
References mwp.
Referenced by gyro_cb().
struct FloatRates ins_mekf_wind_get_body_rates | ( | void | ) |
Definition at line 776 of file ins_mekf_wind.cpp.
Referenced by gyro_cb(), and set_state_from_ins().
struct NedCoor_f ins_mekf_wind_get_pos_ned | ( | void | ) |
Getter/Setter functions.
Definition at line 652 of file ins_mekf_wind.cpp.
References B, ins_mekf_wind_parameters::disable_wind, H, ins_mekf_wind_params, K, MEKF_WIND_abx, MEKF_WIND_bb, MEKF_WIND_px, MEKF_WIND_qx, MEKF_WIND_raoa, MEKF_WIND_rbp, MEKF_WIND_vx, MEKF_WIND_wx, mwp, and skew_sym().
Referenced by gyro_cb(), send_inv_filter(), and set_state_from_ins().
struct FloatQuat ins_mekf_wind_get_quat | ( | void | ) |
Definition at line 748 of file ins_mekf_wind.cpp.
Referenced by gyro_cb(), send_euler(), send_inv_filter(), and set_state_from_ins().
struct FloatRates ins_mekf_wind_get_rates_bias | ( | void | ) |
Definition at line 816 of file ins_mekf_wind.cpp.
Referenced by gyro_cb(), and send_inv_filter().
struct NedCoor_f ins_mekf_wind_get_speed_ned | ( | void | ) |
Definition at line 731 of file ins_mekf_wind.cpp.
Referenced by gyro_cb(), send_inv_filter(), and set_state_from_ins().
struct NedCoor_f ins_mekf_wind_get_wind_ned | ( | void | ) |
Definition at line 776 of file ins_mekf_wind.cpp.
Referenced by gyro_cb(), and send_wind().
void ins_mekf_wind_init | ( | void | ) |
Init function.
Definition at line 308 of file ins_mekf_wind.cpp.
References ins_mekf_wind_parameters::disable_wind, init_mekf_state(), INS_MEKF_WIND_DISABLE_WIND, ins_mekf_wind_params, INS_MEKF_WIND_Q_ACCEL, INS_MEKF_WIND_Q_ACCEL_BIAS, INS_MEKF_WIND_Q_BARO_BIAS, INS_MEKF_WIND_Q_GYRO, INS_MEKF_WIND_Q_RATES_BIAS, INS_MEKF_WIND_Q_WIND, INS_MEKF_WIND_R_AIRSPEED, INS_MEKF_WIND_R_AOA, INS_MEKF_WIND_R_AOS, INS_MEKF_WIND_R_BARO, INS_MEKF_WIND_R_MAG, INS_MEKF_WIND_R_POS, INS_MEKF_WIND_R_POS_Z, INS_MEKF_WIND_R_SPEED, INS_MEKF_WIND_R_SPEED_Z, InsMekfWindPrivate::mag_h, mekf_wind_private, ins_mekf_wind_parameters::Q_accel, ins_mekf_wind_parameters::Q_accel_bias, ins_mekf_wind_parameters::Q_baro_bias, ins_mekf_wind_parameters::Q_gyro, ins_mekf_wind_parameters::Q_rates_bias, ins_mekf_wind_parameters::Q_wind, ins_mekf_wind_parameters::R_airspeed, ins_mekf_wind_parameters::R_aoa, ins_mekf_wind_parameters::R_aos, ins_mekf_wind_parameters::R_baro, ins_mekf_wind_parameters::R_mag, ins_mekf_wind_parameters::R_pos, ins_mekf_wind_parameters::R_pos_z, ins_mekf_wind_parameters::R_speed, and ins_mekf_wind_parameters::R_speed_z.
Referenced by ins_mekf_wind_wrapper_init().
void ins_mekf_wind_propagate | ( | struct FloatRates * | gyro, |
struct FloatVect3 * | acc, | ||
float | dt | ||
) |
Full INS propagation.
Definition at line 350 of file ins_mekf_wind.cpp.
References A, MekfWindInputs::accel, ins_mekf_wind_parameters::disable_wind, gravity(), InsMekfWindPrivate::inputs, INS_MEKF_WIND_P0_WIND, ins_mekf_wind_params, MEKF_WIND_abx, MEKF_WIND_bb, MEKF_WIND_COV_SIZE, mekf_wind_private, MEKF_WIND_px, MEKF_WIND_qabx, MEKF_WIND_qax, MEKF_WIND_qbb, MEKF_WIND_qgp, MEKF_WIND_qrbp, MEKF_WIND_qwx, MEKF_WIND_qx, MEKF_WIND_rbp, MEKF_WIND_vx, MEKF_WIND_wx, MEKF_WIND_wy, MEKF_WIND_wz, mwp, FloatRates::p, FloatRates::q, quat_add(), quat_smul(), FloatRates::r, MekfWindInputs::rates, skew_sym(), FloatVect3::x, FloatVect3::y, and FloatVect3::z.
Referenced by gyro_cb().
void ins_mekf_wind_propagate_ahrs | ( | struct FloatRates * | gyro, |
struct FloatVect3 * | acc, | ||
float | dt | ||
) |
AHRS-only propagation + accel correction.
Definition at line 422 of file ins_mekf_wind.cpp.
References A, MekfWindInputs::accel, gravity(), H, InsMekfWindPrivate::inputs, K, mekf_wind_private, MEKF_WIND_qgp, MEKF_WIND_qrbp, MEKF_WIND_qx, MEKF_WIND_rbp, MEKF_WIND_rmx, mwp, FloatRates::p, FloatRates::q, quat_add(), quat_smul(), FloatRates::r, MekfWindInputs::rates, skew_sym(), FloatVect3::x, FloatVect3::y, and FloatVect3::z.
Referenced by gyro_cb().
void ins_mekf_wind_reset | ( | void | ) |
Definition at line 343 of file ins_mekf_wind.cpp.
References init_mekf_state().
void ins_mekf_wind_set_mag_h | ( | const struct FloatVect3 * | mag_h | ) |
Definition at line 335 of file ins_mekf_wind.cpp.
References InsMekfWindPrivate::mag_h, and mekf_wind_private.
Referenced by geo_mag_cb(), and ins_mekf_wind_wrapper_init().
void ins_mekf_wind_set_pos_ned | ( | struct NedCoor_f * | p | ) |
Definition at line 731 of file ins_mekf_wind.cpp.
Referenced by gps_cb().
void ins_mekf_wind_set_quat | ( | struct FloatQuat * | quat | ) |
Definition at line 776 of file ins_mekf_wind.cpp.
void ins_mekf_wind_set_speed_ned | ( | struct NedCoor_f * | s | ) |
Definition at line 748 of file ins_mekf_wind.cpp.
Referenced by gps_cb().
void ins_mekf_wind_update_airspeed | ( | float | airspeed | ) |
Definition at line 614 of file ins_mekf_wind.cpp.
References ins_mekf_wind_parameters::disable_wind, H, ins_mekf_wind_params, K, MEKF_WIND_abx, MEKF_WIND_bb, MEKF_WIND_px, MEKF_WIND_qx, MEKF_WIND_ras, MEKF_WIND_rbp, MEKF_WIND_vx, MEKF_WIND_wx, mwp, and skew_sym().
Referenced by airspeed_cb(), and pressure_diff_cb().
void ins_mekf_wind_update_baro | ( | float | baro_alt | ) |
Definition at line 541 of file ins_mekf_wind.cpp.
References baro_alt, ins_mekf_wind_parameters::disable_wind, H, ins_mekf_wind_params, K, MEKF_WIND_abx, MEKF_WIND_bb, MEKF_WIND_px, MEKF_WIND_pz, MEKF_WIND_qx, MEKF_WIND_rb, MEKF_WIND_rbp, MEKF_WIND_vx, MEKF_WIND_wx, and mwp.
Referenced by baro_cb().
void ins_mekf_wind_update_incidence | ( | float | aoa, |
float | aos | ||
) |
Definition at line 652 of file ins_mekf_wind.cpp.
Referenced by incidence_cb().
void ins_mekf_wind_update_mag | ( | struct FloatVect3 * | mag, |
bool | attitude_only | ||
) |
Definition at line 501 of file ins_mekf_wind.cpp.
References ins_mekf_wind_parameters::disable_wind, H, ins_mekf_wind_params, K, MEKF_WIND_abx, MEKF_WIND_bb, MEKF_WIND_px, MEKF_WIND_qx, MEKF_WIND_rbp, MEKF_WIND_rmx, MEKF_WIND_vx, MEKF_WIND_wx, mwp, skew_sym(), FloatVect3::x, FloatVect3::y, and FloatVect3::z.
Referenced by mag_cb().
void ins_mekf_wind_update_params | ( | void | ) |
Definition at line 846 of file ins_mekf_wind.cpp.
References ins_mekf_wind_params, mekf_wind_private, MEKF_WIND_qabx, MEKF_WIND_qaby, MEKF_WIND_qabz, MEKF_WIND_qax, MEKF_WIND_qay, MEKF_WIND_qaz, MEKF_WIND_qbb, MEKF_WIND_qgp, MEKF_WIND_qgq, MEKF_WIND_qgr, MEKF_WIND_qrbp, MEKF_WIND_qrbq, MEKF_WIND_qrbr, MEKF_WIND_qwx, MEKF_WIND_qwy, MEKF_WIND_qwz, MEKF_WIND_raoa, MEKF_WIND_raos, MEKF_WIND_ras, MEKF_WIND_rb, MEKF_WIND_rmx, MEKF_WIND_rmy, MEKF_WIND_rmz, MEKF_WIND_rpx, MEKF_WIND_rpy, MEKF_WIND_rpz, MEKF_WIND_rvx, MEKF_WIND_rvy, MEKF_WIND_rvz, InsMekfWindPrivate::Q, ins_mekf_wind_parameters::Q_accel, ins_mekf_wind_parameters::Q_accel_bias, ins_mekf_wind_parameters::Q_baro_bias, ins_mekf_wind_parameters::Q_gyro, ins_mekf_wind_parameters::Q_rates_bias, ins_mekf_wind_parameters::Q_wind, InsMekfWindPrivate::R, ins_mekf_wind_parameters::R_airspeed, ins_mekf_wind_parameters::R_aoa, ins_mekf_wind_parameters::R_aos, ins_mekf_wind_parameters::R_baro, ins_mekf_wind_parameters::R_mag, ins_mekf_wind_parameters::R_pos, ins_mekf_wind_parameters::R_pos_z, ins_mekf_wind_parameters::R_speed, and ins_mekf_wind_parameters::R_speed_z.
Referenced by init_mekf_state().
void ins_mekf_wind_update_pos_speed | ( | struct FloatVect3 * | pos, |
struct FloatVect3 * | speed | ||
) |
Definition at line 575 of file ins_mekf_wind.cpp.
References ins_mekf_wind_parameters::disable_wind, H, ins_mekf_wind_params, K, MEKF_WIND_abx, MEKF_WIND_bb, MEKF_WIND_px, MEKF_WIND_qx, MEKF_WIND_rbp, MEKF_WIND_rvx, MEKF_WIND_vx, MEKF_WIND_wx, mwp, FloatVect3::x, FloatVect3::y, and FloatVect3::z.
Referenced by gps_cb().
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Definition at line 280 of file ins_mekf_wind.cpp.
Referenced by ins_mekf_wind_propagate(), and ins_mekf_wind_propagate_ahrs().
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Definition at line 284 of file ins_mekf_wind.cpp.
Referenced by ins_mekf_wind_propagate(), and ins_mekf_wind_propagate_ahrs().
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build skew symetric matrix from vector m = [ 0, -v(2), v(1) ] [ v(2), 0, -v(0) ] [ -v(1), v(0), 0 ]
Definition at line 294 of file ins_mekf_wind.cpp.
References simple_quad_sim::m.
Referenced by ins_mekf_wind_get_pos_ned(), ins_mekf_wind_propagate(), ins_mekf_wind_propagate_ahrs(), ins_mekf_wind_update_airspeed(), and ins_mekf_wind_update_mag().
struct ins_mekf_wind_parameters ins_mekf_wind_params |
Definition at line 89 of file ins_mekf_wind.cpp.
Referenced by ins_mekf_wind_get_pos_ned(), ins_mekf_wind_init(), ins_mekf_wind_propagate(), ins_mekf_wind_update_airspeed(), ins_mekf_wind_update_baro(), ins_mekf_wind_update_mag(), ins_mekf_wind_update_params(), and ins_mekf_wind_update_pos_speed().
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Definition at line 89 of file ins_mekf_wind.cpp.
Referenced by init_mekf_state(), ins_mekf_wind_init(), ins_mekf_wind_propagate(), ins_mekf_wind_propagate_ahrs(), ins_mekf_wind_set_mag_h(), and ins_mekf_wind_update_params().