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AP_NavEKF: implemented getRotationBodyToNED()
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@ -2110,4 +2110,11 @@ void NavEKF::calcEarthRateNED(Vector3f &omega, float latitude) const
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omega.z = -earthRate*sinf(latitude);
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omega.z = -earthRate*sinf(latitude);
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}
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}
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void NavEKF::getRotationBodyToNED(Matrix3f &mat) const
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{
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Quaternion q(states[0], states[1], states[2], states[3]);
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q.rotation_matrix(mat);
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}
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#endif // HAL_CPU_CLASS
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#endif // HAL_CPU_CLASS
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