AP_NavEKF3: Improve variable names and documentation
Also remove unnecessary calculation of innov * gain
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@ -562,14 +562,15 @@ void NavEKF3_core::CalcRangeBeaconPosDownOffset(float obsVar, Vector3f &vehicleP
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// calculate the Kalman gain
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gain = (bcnPosOffsetMaxVar * obsDeriv) / innovVar;
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// calculate a filtered state change magnitude to be used to select between the high or low offset
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float stateChange = innov * gain;
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OffsetMaxInnovFilt = (1.0f - filtAlpha) * OffsetMaxInnovFilt + fminf(fabsf(filtAlpha * stateChange) , 1.0f);
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maxOffsetStateChangeFilt = (1.0f - filtAlpha) * maxOffsetStateChangeFilt + fminf(fabsf(filtAlpha * stateChange) , 1.0f);
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// Reject range innovation spikes using a 5-sigma threshold unless aligning
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if ((sq(innov) < sq(innovGateWidth) * innovVar) || aligning) {
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// state update
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bcnPosDownOffsetMax -= innov * gain;
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bcnPosDownOffsetMax -= stateChange;
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// covariance update
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bcnPosOffsetMaxVar -= gain * obsDeriv * bcnPosOffsetMaxVar;
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@ -602,7 +603,7 @@ void NavEKF3_core::CalcRangeBeaconPosDownOffset(float obsVar, Vector3f &vehicleP
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// calculate a filtered state change magnitude to be used to select between the high or low offset
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float stateChange = innov * gain;
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OffsetMinInnovFilt = (1.0f - filtAlpha) * OffsetMinInnovFilt + fminf(fabsf(filtAlpha * stateChange) , 1.0f);
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minOffsetStateChangeFilt = (1.0f - filtAlpha) * minOffsetStateChangeFilt + fminf(fabsf(filtAlpha * stateChange) , 1.0f);
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// Reject range innovation spikes using a 5-sigma threshold unless aligning
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if ((sq(innov) < sq(innovGateWidth) * innovVar) || aligning) {
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@ -625,9 +626,9 @@ void NavEKF3_core::CalcRangeBeaconPosDownOffset(float obsVar, Vector3f &vehicleP
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// calculate the innovation for the main filter using the offset that is most stable
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// apply hysteresis to prevent rapid switching
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if (!usingMinHypothesis && (OffsetMinInnovFilt < (0.8f * OffsetMaxInnovFilt))) {
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if (!usingMinHypothesis && (minOffsetStateChangeFilt < (0.8f * maxOffsetStateChangeFilt))) {
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usingMinHypothesis = true;
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} else if (usingMinHypothesis && (OffsetMaxInnovFilt < (0.8f * OffsetMinInnovFilt))) {
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} else if (usingMinHypothesis && (maxOffsetStateChangeFilt < (0.8f * minOffsetStateChangeFilt))) {
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usingMinHypothesis = false;
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}
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if (usingMinHypothesis) {
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@ -353,10 +353,10 @@ void NavEKF3_core::InitialiseVariables()
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minBcnPosD = 0.0f;
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bcnPosDownOffsetMax = 0.0f;
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bcnPosOffsetMaxVar = 0.0f;
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OffsetMaxInnovFilt = 0.0f;
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maxOffsetStateChangeFilt = 0.0f;
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bcnPosDownOffsetMin = 0.0f;
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bcnPosOffsetMinVar = 0.0f;
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OffsetMinInnovFilt = 0.0f;
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minOffsetStateChangeFilt = 0.0f;
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rngBcnFuseDataReportIndex = 0;
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memset(&rngBcnFusionReport, 0, sizeof(rngBcnFusionReport));
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bcnPosOffsetNED.zero();
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@ -1091,11 +1091,11 @@ private:
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float bcnPosDownOffsetMax; // Vertical position offset of the beacon constellation origin relative to the EKF origin (m)
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float bcnPosOffsetMaxVar; // Variance of the bcnPosDownOffsetMax state (m)
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float OffsetMaxInnovFilt; // Filtered magnitude of the range innovations using bcnPosOffsetHigh
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float maxOffsetStateChangeFilt; // Filtered magnitude of the change in bcnPosOffsetHigh
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float bcnPosDownOffsetMin; // Vertical position offset of the beacon constellation origin relative to the EKF origin (m)
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float bcnPosOffsetMinVar; // Variance of the bcnPosDownOffsetMin state (m)
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float OffsetMinInnovFilt; // Filtered magnitude of the range innovations using bcnPosOffsetLow
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float minOffsetStateChangeFilt; // Filtered magnitude of the change in bcnPosOffsetLow
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Vector3f bcnPosOffsetNED; // NED position of the beacon origin in earth frame (m)
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bool bcnOriginEstInit; // True when the beacon origin has been initialised
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