mirror of https://github.com/ArduPilot/ardupilot
AP_NavEKF: Update EKF optical flow data logging
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@ -3668,16 +3668,17 @@ bool NavEKF::getHAGL(float &HAGL) const
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}
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// return data for debugging optical flow fusion
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void NavEKF::getFlowDebug(float &scaleFactor, float &gndPos, float &flowInnovX, float &flowInnovY, float &augFlowInnovX, float &augFlowInnovY, float &rngInnov, float &range) const
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void NavEKF::getFlowDebug(float &scaleFactor, float &estHAGL, float &flowInnovX, float &flowInnovY, float &flowVarX, float &flowVarY, float &rngInnov, float &range, float &gndOffsetErr) const
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{
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scaleFactor = flowStates[0];
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gndPos = flowStates[1];
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estHAGL = flowStates[1] - state.position.z;
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flowInnovX = innovOptFlow[0];
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flowInnovY = innovOptFlow[1];
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augFlowInnovX = auxFlowObsInnov[0];
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augFlowInnovY = auxFlowObsInnov[1];
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flowVarX = flowTestRatio[0];
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flowVarY = flowTestRatio[1];
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rngInnov = innovRng;
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range = rngMea;
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gndOffsetErr = sqrtf(Popt[1][1]); // note Popt[1][1] is constrained to be non-negative in RunAuxiliaryEKF()
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}
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// calculate whether the flight vehicle is on the ground or flying from height, airspeed and GPS speed
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@ -171,7 +171,7 @@ public:
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void writeOptFlowMeas(uint8_t &rawFlowQuality, Vector2f &rawFlowRates, Vector2f &rawGyroRates, uint32_t &msecFlowMeas, uint8_t &rangeHealth, float &rawSonarRange);
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// return data for debugging optical flow fusion
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void getFlowDebug(float &scaleFactor, float &gndPos, float &flowInnovX, float &flowInnovY, float &augFlowInnovX, float &augFlowInnovY, float &rngInnov, float &range) const;
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void getFlowDebug(float &scaleFactor, float &gndPos, float &flowInnovX, float &flowInnovY, float &flowVarX, float &flowVarY, float &rngInnov, float &range, float &gndOffsetErr) const;
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/*
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return the filter fault status as a bitmasked integer
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