Paul Riseborough 8dc6354a54 AP_NavEKF: Prevent touchdown baro errors tripping height innovation check ... Ground effect baro errors can cause a spike in height innovation on disarming if ground effect compensation was used during the landing. This causes a transient AHRS fault message if this innovation is outside the pre-arm check limits. Resetting the vertical position state to the measured height after disarming prevents this.		2015-05-01 16:37:23 +09:00
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Models	AP_NavEKF: Add Matlab derivations and simulations behind small EKF	2015-04-10 11:07:21 +09:00
AP_Nav_Common.h	AP_NavEKF: Add takeoff and touchdown expected to reported filter status	2015-05-01 16:37:19 +09:00
AP_NavEKF.cpp	AP_NavEKF: Prevent touchdown baro errors tripping height innovation check	2015-05-01 16:37:23 +09:00
AP_NavEKF.h	AP_NavEKF: use quaternion functions to apply IMU delta angles	2015-05-01 16:37:22 +09:00
AP_SmallEKF.cpp	AP_SmallEKF: increase start-up time of the SmallEKF	2015-04-21 21:45:51 +09:00
AP_SmallEKF.h	AP_SmallEKF: add function to report if the EKF is stable	2015-04-21 21:45:29 +09:00