mirror of https://github.com/ArduPilot/ardupilot
AP_NavEKF2: Use measurement uncertainties to initialise covariance
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@ -359,11 +359,11 @@ void NavEKF2_core::CovarianceInit()
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P[1][1] = 0.1f;
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P[1][1] = 0.1f;
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P[2][2] = 0.1f;
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P[2][2] = 0.1f;
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// velocities
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// velocities
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P[3][3] = sq(0.7f);
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P[3][3] = sq(frontend->_gpsHorizVelNoise);
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P[4][4] = P[3][3];
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P[4][4] = P[3][3];
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P[5][5] = sq(0.7f);
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P[5][5] = sq(frontend->_gpsVertVelNoise);
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// positions
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// positions
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P[6][6] = sq(15.0f);
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P[6][6] = sq(frontend->_gpsHorizPosNoise);
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P[7][7] = P[6][6];
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P[7][7] = P[6][6];
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P[8][8] = sq(frontend->_baroAltNoise);
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P[8][8] = sq(frontend->_baroAltNoise);
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// gyro delta angle biases
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// gyro delta angle biases
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