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https://github.com/ArduPilot/ardupilot
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AP_NavEKF: improved covariance matrix numerical stability protection
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@ -978,7 +978,19 @@ void NavEKF::CovariancePrediction()
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}
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}
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FixCovarianceErrors();
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// Copy to output whilst forcing symmetry to prevent ill-conditioning
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// of the matrix
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for (uint8_t i=0; i<=20; i++) P[i][i] = nextP[i][i];
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for (uint8_t i=1; i<=20; i++)
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{
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for (uint8_t j=0; j<=i-1; j++)
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{
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P[i][j] = 0.5f*(nextP[i][j] + nextP[j][i]);
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P[j][i] = P[i][j];
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}
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}
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ConstrainVariances();
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perf_end(_perf_CovariancePrediction);
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}
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@ -1209,6 +1221,12 @@ void NavEKF::FuseVelPosNED()
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}
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}
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}
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// force the covariance matrix to me symmetrical and limit the variances to prevent
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// ill-condiioning.
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ForceSymmetry();
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ConstrainVariances();
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perf_end(_perf_FuseVelPosNED);
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}
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@ -1513,6 +1531,12 @@ void NavEKF::FuseMagnetometer()
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magFusePerformed = false;
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magFuseRequired = false;
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}
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// force the covariance matrix to me symmetrical and limit the variances to prevent
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// ill-condiioning.
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ForceSymmetry();
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ConstrainVariances();
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perf_end(_perf_FuseMagnetometer);
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}
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@ -1636,6 +1660,12 @@ void NavEKF::FuseAirspeed()
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}
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}
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}
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// force the covariance matrix to me symmetrical and limit the variances to prevent
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// ill-condiioning.
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ForceSymmetry();
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ConstrainVariances();
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perf_end(_perf_FuseAirspeed);
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}
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@ -1801,26 +1831,29 @@ void NavEKF::CovarianceInit()
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P[20][20] = P[18][18];
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}
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void NavEKF::FixCovarianceErrors()
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void NavEKF::ForceSymmetry()
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{
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// Force symmetry on the covariance matrix to prevent ill-conditioning
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// of the matrix which would cause the filter to blow-up
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for (uint8_t i=0; i<=20; i++) P[i][i] = nextP[i][i];
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for (uint8_t i=1; i<=20; i++)
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{
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for (uint8_t j=0; j<=i-1; j++)
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{
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float temp = 0.5f*(nextP[i][j] + nextP[j][i]);
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float temp = 0.5f*(P[i][j] + P[j][i]);
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P[i][j] = temp;
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P[j][i] = temp;
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}
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}
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}
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void NavEKF::ConstrainVariances()
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{
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// Constrain variances to be within set limits
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for (uint8_t i=0; i<=3; i++) constrain_float(P[1][1],0.0f,0.1f);
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for (uint8_t i=4; i<=6; i++) constrain_float(P[1][1],0.0f,1000.0f);
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for (uint8_t i=7; i<=9; i++) constrain_float(P[1][1],0.0f,1.0e6f);
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for (uint8_t i=10; i<=12; i++) constrain_float(P[1][1],0.0f,sq(0.0175 * dtIMUAvg)); // 60 deg/min bias error
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for (uint8_t i=13; i<=14; i++) constrain_float(P[1][1],0.0f,400.0f);
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for (uint8_t i=4; i<=6; i++) constrain_float(P[1][1],0.0f,1.0e3f);
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for (uint8_t i=7; i<=9; i++) constrain_float(P[1][1],0.0f,1.0e5f);
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for (uint8_t i=10; i<=12; i++) constrain_float(P[1][1],0.0f,sq(0.0175 * dtIMUAvg));
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for (uint8_t i=13; i<=14; i++) constrain_float(P[1][1],0.0f,1.0e3f);
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for (uint8_t i=15; i<=20; i++) constrain_float(P[1][1],0.0f,1.0f);
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}
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@ -131,7 +131,9 @@ private:
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void CovariancePrediction();
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void FixCovarianceErrors();
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void ForceSymmetry();
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void ConstrainVariances();
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void FuseVelPosNED();
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