ekf2-mag: add inclination check

This commit is contained in:
bresch
2023-07-24 10:16:37 -04:00
committed by Daniel Agar
parent e4a16bfc80
commit 357bf024f6
9 changed files with 122 additions and 6 deletions
+1
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@@ -494,6 +494,7 @@ struct parameters {
int32_t synthesize_mag_z{0};
int32_t mag_check{0};
float mag_check_strength_tolerance_gs{0.2f};
float mag_check_inclination_tolerance_deg{20.f};
// Parameters used to control when yaw is reset to the EKF-GSF yaw estimator value
float EKFGSF_tas_default{15.0f}; ///< default airspeed value assumed during fixed wing flight if no airspeed measurement available (m/s)
+2 -2
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@@ -216,10 +216,10 @@ public:
// Get the value of magnetic declination in degrees to be saved for use at the next startup
// Returns true when the declination can be saved
// At the next startup, set param.mag_declination_deg to the value saved
bool get_mag_decl_deg(float *val) const
bool get_mag_decl_deg(float &val) const
{
if (_NED_origin_initialised && (_params.mag_declination_source & GeoDeclinationMask::SAVE_GEO_DECL)) {
*val = math::degrees(_mag_declination_gps);
val = math::degrees(_mag_declination_gps);
return true;
} else {
+22
View File
@@ -471,6 +471,28 @@ bool Ekf::checkMagField(const Vector3f &mag_sample)
}
}
const Vector3f mag_earth = _R_to_earth * mag_sample;
const float mag_inclination = asin(mag_earth(2) / fmaxf(mag_earth.norm(), 1e-4f));
if (_params.mag_check & static_cast<int32_t>(MagCheckMask::INCLINATION)) {
if (PX4_ISFINITE(_mag_inclination_gps)) {
const float inc_tol_rad = radians(_params.mag_check_inclination_tolerance_deg);
const float inc_error_rad = wrap_pi(mag_inclination - _mag_inclination_gps);
if (fabsf(inc_error_rad) > inc_tol_rad) {
_control_status.flags.mag_field_disturbed = true;
is_check_failing = true;
}
} else if (_params.mag_check & static_cast<int32_t>(MagCheckMask::FORCE_WMM)) {
is_check_failing = true;
} else {
// No check possible when the global position is unknown
// TODO: add parameter to remember the inclination between boots
}
}
if (is_check_failing || (_time_last_mag_check_failing == 0)) {
_time_last_mag_check_failing = _time_delayed_us;
}