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PX4-Autopilot/EKF
Paul Riseborough 1540e937b1 EKF: Improve tilt alignment monitoring
Convert quaternion covariances into an angular alignment variance vector and discard the z component so that yaw uncertainty does not affect the result.
2016-05-17 11:17:24 +10:00
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2016-04-16 21:46:50 -04:00
2016-05-15 20:36:51 +10:00
2016-05-17 11:17:24 +10:00
2016-02-25 08:17:50 +11:00