Tom Pittenger e987173ffb AP_NavEKF: float to double promotion via tan instead of tanf		2015-05-16 08:21:49 +10:00
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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: Add pre-arm check for horizontal inertial errors	2015-05-15 10:35:25 +09:00
AP_NavEKF.h	AP_NavEKF: Prevent EKF yaw errors due to fast yaw spins	2015-05-08 16:47:31 +09:00
AP_SmallEKF.cpp	AP_NavEKF: float to double promotion via tan instead of tanf	2015-05-16 08:21:49 +10:00
AP_SmallEKF.h	AP_SmallEKF: add function to report if the EKF is stable	2015-04-21 21:45:29 +09:00