mirror of https://github.com/ArduPilot/ardupilot
AP_NavEKF : Fix bug in scaling of initial Z accel bias state variance
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@ -3837,7 +3837,7 @@ void NavEKF::CovarianceInit()
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P[11][11] = P[10][10];
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P[12][12] = P[10][10];
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// Z delta velocity bias
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P[13][13] = sq(radians(INIT_ACCEL_BIAS_UNCERTAINTY * dtIMU));;
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P[13][13] = sq(INIT_ACCEL_BIAS_UNCERTAINTY * dtIMU);
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// wind velocities
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P[14][14] = 0.0f;
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P[15][15] = P[14][14];
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