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synced 2026-04-14 10:07:39 +08:00
Made fault tolerances adjustable.
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@ -98,6 +98,8 @@ KalmanNav::KalmanNav(SuperBlock *parent, const char *name) :
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_rAccel(this, "R_ACCEL"),
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_magDip(this, "MAG_DIP"),
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_magDec(this, "MAG_DEC"),
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_faultPos(this, "FAULT_POS"),
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_faultAtt(this, "FAULT_ATT"),
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_positionInitialized(false)
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{
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using namespace math;
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@ -601,7 +603,7 @@ void KalmanNav::correctAtt()
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// fault detection
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float beta = y.dot(S.inverse() * y);
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if (beta > 1000.0f) {
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if (beta > _faultAtt.get()) {
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printf("fault in attitude: beta = %8.4f\n", (double)beta);
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printf("y:\n"); y.print();
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}
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@ -679,7 +681,7 @@ void KalmanNav::correctPos()
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// fault detetcion
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float beta = y.dot(S.inverse() * y);
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if (beta > 1000.0f) {
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if (beta > _faultPos.get()) {
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printf("fault in gps: beta = %8.4f\n", (double)beta);
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printf("Y/N: vN: %8.4f, vE: %8.4f, lat: %8.4f, lon: %8.4f, alt: %8.4f\n",
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double(y(0) / noiseVel),
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@ -159,6 +159,8 @@ protected:
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control::BlockParam<float> _rAccel; /**< accelerometer measurement noise */
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control::BlockParam<float> _magDip; /**< magnetic inclination with level */
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control::BlockParam<float> _magDec; /**< magnetic declination, clockwise rotation */
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control::BlockParam<float> _faultPos; /**< fault detection threshold for position */
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control::BlockParam<float> _faultAtt; /**< fault detection threshold for attitude */
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// status
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bool _positionInitialized; /**< status, if position has been init. */
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// accessors
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@ -10,3 +10,5 @@ PARAM_DEFINE_FLOAT(KF_R_GPS_ALT, 1.0f);
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PARAM_DEFINE_FLOAT(KF_R_ACCEL, 1.0f);
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PARAM_DEFINE_FLOAT(KF_MAG_DIP, 60.0f);
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PARAM_DEFINE_FLOAT(KF_MAG_DEC, 0.0f);
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PARAM_DEFINE_FLOAT(KF_FAULT_POS, 1000.0f);
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PARAM_DEFINE_FLOAT(KF_FAULT_ATT, 10.0f);
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