ardupilot/libraries/AP_NavEKF
Paul Riseborough b1d8805114 AP_NavEKF: Reduce takeoff detection sensitivity
This patch reworks the in-air transition criteria to reduce the likelihood of false positives and to ensure that there will be enough ground speed to make the heading check work reliably.
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: Reduce takeoff detection sensitivity 2015-05-19 20:35:52 +10:00
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