Paul Riseborough 1ecc206eee AP_NavEKF2: Allow use in planes without a magnetometer ... Implements the following techniques to enable planes to operate without magnetometers. 1) When on ground with mag use inhibited, a synthetic heading equal to current heading is fused to prevent uncontrolled covariance growth. 2) When transitioning to in-flight, the delta between inertial and GPS velocity vector is used to align the yaw. 3) The yaw gyro bias state variance is reset following an in-flight heading reset to enable the yaw gyro bias to be learned faster.		2016-04-15 08:31:47 +10:00
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AP_NavEKF2_AirDataFusion.cpp	Global: rename min and max macros to uppercase	2015-12-01 16:28:09 -02:00
AP_NavEKF2_Buffer.h	AP_NavEKF2: Rework measurement buffer refactor	2015-11-23 19:42:06 +11:00
AP_NavEKF2_Control.cpp	AP_NavEKF2: Improvements to non-GPS performance	2016-02-18 08:53:41 +09:00
AP_NavEKF2_core.cpp	AP_NavEKF2: Allow use in planes without a magnetometer	2016-04-15 08:31:47 +10:00
AP_NavEKF2_core.h	AP_NavEKF2: Allow use in planes without a magnetometer	2016-04-15 08:31:47 +10:00
AP_NavEKF2_MagFusion.cpp	AP_NavEKF2: Allow use in planes without a magnetometer	2016-04-15 08:31:47 +10:00
AP_NavEKF2_Measurements.cpp	AP_NavEKF2: use get_delta_angle_dt() API	2016-01-19 09:50:22 +11:00
AP_NavEKF2_OptFlowFusion.cpp	Global: rename min and max macros to uppercase	2015-12-01 16:28:09 -02:00
AP_NavEKF2_Outputs.cpp	AP_NavEKF2: Send correct data over mavlink status message	2016-02-01 10:02:22 +09:00
AP_NavEKF2_PosVelFusion.cpp	AP_NavEKF2: Do not use GPS height if GPS accuracy is poor	2016-03-01 15:13:13 +09:00
AP_NavEKF2_VehicleStatus.cpp	Global: rename min and max macros to uppercase	2015-12-01 16:28:09 -02:00
AP_NavEKF2.cpp	AP_NavEKF2: Improvements to non-GPS performance	2016-02-18 08:53:41 +09:00
AP_NavEKF2.h	AP_NavEKF2: replace header guard with pragma once	2016-03-16 18:40:42 +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