Andrew Tridgell 411a96b4b3 AP_NavEKF: take at most 30s to accept DCM attitude ... velocity noise on the GPS can cause DCM to take a long time to converge. If it takes longer than 30s then allow EKF to start		2015-05-20 15:22:15 +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_NavEKF.cpp	AP_NavEKF: take at most 30s to accept DCM attitude	2015-05-20 15:22:15 +10:00
AP_NavEKF.h	AP_NavEKF: Enforce alignment of realigned earth mag field with declination	2015-05-19 20:35:52 +10:00
AP_Nav_Common.h	AP_NavEKF: added using_gps status bit	2015-05-17 21:24:57 +10:00
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