Paul Riseborough 2193103586 AP_NavEKF: Reduce time to switch after an IMU fault ... This revised threshold value is still double the maximum that has been observed in flight logs so far with healthy sensors The previous value was too slow to switch for sudden IMU gyro faults We can afford an ocasional false trigger becasue the front end will only select another instance if it is healthy and has lower errors		2015-11-18 20:17:00 +09:00
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AP_NavEKF2_AirDataFusion.cpp	AP_NavEKF2: Increase resolution of innovation consistency gate parameters	2015-11-18 11:39:53 +11:00
AP_NavEKF2_Control.cpp	AP_NavEKF2: Fix plane in-flight yaw reset	2015-11-16 09:05:42 +11:00
AP_NavEKF2_core.cpp	AP_NavEKF2: Rework selection of height measurements for fusion	2015-11-18 11:18:42 +11:00
AP_NavEKF2_core.h	AP_NavEKF2: Make magnetometer data available status global	2015-11-18 11:18:46 +11:00
AP_NavEKF2_MagFusion.cpp	AP_NavEKF2: fix bug in performance timer	2015-11-18 20:16:58 +09:00
AP_NavEKF2_Measurements.cpp	AP_NavEKF2: Rework selection of height measurements for fusion	2015-11-18 11:18:42 +11:00
AP_NavEKF2_OptFlowFusion.cpp	AP_NavEKF2: Increase resolution of innovation consistency gate parameters	2015-11-18 11:39:53 +11:00
AP_NavEKF2_Outputs.cpp	AP_NavEKF: Reduce time to switch after an IMU fault	2015-11-18 20:17:00 +09:00
AP_NavEKF2_PosVelFusion.cpp	AP_NavEKF2: Increase resolution of innovation consistency gate parameters	2015-11-18 11:39:53 +11:00
AP_NavEKF2_VehicleStatus.cpp	AP_NavEKF2: Rework selection of height measurements for fusion	2015-11-18 11:18:42 +11:00
AP_NavEKF2.cpp	AP_NavEKF2: Prevent airspeed faults from causing excessive loss of accuracy	2015-11-18 11:39:54 +11:00
AP_NavEKF2.h	AP_NavEKF2: Increase resolution of innovation consistency gate parameters	2015-11-18 11:39:53 +11:00
AP_NavEKF_GyroBias.cpp	AP_NavEKF2: use common header for optimisation level and irq disable	2015-10-20 15:21:40 +11:00