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c1c5e3598a
Ardupilot2/libraries/AP_NavEKF
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Paul Riseborough c1c5e3598a AP_NavEKF: Enforce alignment of realigned earth mag field with declination 
This prevents bad inertial or GPS data combined with the post takeoff heading alignment check used by plane from resulting in earth field states that have an incorrect declination
2015-05-19 20:35:52 +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: added using_gps status bit 2015-05-17 21:24:57 +10:00
AP_NavEKF.cpp AP_NavEKF: Enforce alignment of realigned earth mag field with declination 2015-05-19 20:35:52 +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_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