Paul Riseborough 5d70854c08 AP_NavEKF: Fix minor bug in calculation of innovation variance ... the innovation variance for GPS should be the sum of squares of the state and measurement uncertainty.		2015-04-15 17:32:46 +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 pred_horiz_pos flags to filter status	2015-01-09 10:51:23 +11:00
AP_NavEKF.cpp	AP_NavEKF: Fix minor bug in calculation of innovation variance	2015-04-15 17:32:46 +09:00
AP_NavEKF.h	AP_NavEKF: Fail absolute position status if GPS repeatedly rejected	2015-04-15 17:32:44 +09:00
AP_SmallEKF.cpp	AP_NavEKF: use compass->last_update_usec()	2015-03-14 12:31:39 +11:00
AP_SmallEKF.h	AP_NavEKF: Publish small EKF quaternion and gyro bias outputs	2015-02-03 09:49:16 +11:00