mirror of https://github.com/ArduPilot/ardupilot
AP_NavEKF : remove debug code
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@ -52,10 +52,6 @@ void NavEKF::InitialiseFilter(void)
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{
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{
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// Calculate initial filter quaternion states from ahrs solution
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// Calculate initial filter quaternion states from ahrs solution
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Quaternion initQuat;
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Quaternion initQuat;
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//debug code
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// ahrsEul[0] = -2.6f*DEG_TO_RAD;//_ahrs.roll;
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// ahrsEul[1] = +3.4f*DEG_TO_RAD;//_ahrs.pitch;
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// ahrsEul[2] = -42.0f*DEG_TO_RAD;//_ahrs.yaw;
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ahrsEul[0] = _ahrs.roll;
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ahrsEul[0] = _ahrs.roll;
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ahrsEul[1] = _ahrs.pitch;
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ahrsEul[1] = _ahrs.pitch;
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ahrsEul[2] = _ahrs.yaw;
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ahrsEul[2] = _ahrs.yaw;
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@ -144,8 +140,6 @@ void NavEKF::UpdateFilter()
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StoreStates();
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StoreStates();
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// Check if on ground - status is used by covariance prediction
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// Check if on ground - status is used by covariance prediction
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OnGroundCheck();
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OnGroundCheck();
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//debug code
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onGround = false;
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// sum delta angles and time used by covariance prediction
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// sum delta angles and time used by covariance prediction
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summedDelAng = summedDelAng + correctedDelAng;
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summedDelAng = summedDelAng + correctedDelAng;
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summedDelVel = summedDelVel + correctedDelVel;
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summedDelVel = summedDelVel + correctedDelVel;
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