AP_NavEKF3: remove unused quat2Tbn method
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@ -1544,13 +1544,6 @@ void NavEKF3_core::StoreQuatRotate(const Quaternion &deltaQuat)
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outputDataDelayed.quat = outputDataDelayed.quat*deltaQuat;
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outputDataDelayed.quat = outputDataDelayed.quat*deltaQuat;
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}
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}
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// calculate nav to body quaternions from body to nav rotation matrix
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void NavEKF3_core::quat2Tbn(Matrix3f &Tbn, const Quaternion &quat) const
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{
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// Calculate the body to nav cosine matrix
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quat.rotation_matrix(Tbn);
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}
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// force symmetry on the covariance matrix to prevent ill-conditioning
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// force symmetry on the covariance matrix to prevent ill-conditioning
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void NavEKF3_core::ForceSymmetry()
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void NavEKF3_core::ForceSymmetry()
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{
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{
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@ -715,9 +715,6 @@ private:
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// Rotate the stored output quaternion history through a quaternion rotation
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// Rotate the stored output quaternion history through a quaternion rotation
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void StoreQuatRotate(const Quaternion &deltaQuat);
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void StoreQuatRotate(const Quaternion &deltaQuat);
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// calculate nav to body quaternions from body to nav rotation matrix
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void quat2Tbn(Matrix3f &Tbn, const Quaternion &quat) const;
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// calculate the NED earth spin vector in rad/sec
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// calculate the NED earth spin vector in rad/sec
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void calcEarthRateNED(Vector3f &omega, int32_t latitude) const;
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void calcEarthRateNED(Vector3f &omega, int32_t latitude) const;
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