Paul Riseborough 6523481c76 AP_NavEKF2: Improve tracking accuracy of output predictor ... Automatically use the highest gain consistent with a 5% overshoot to minimise RMS tracking errors. Provide an alternative correction method for the position and velocity states that allows the user to specify the time-constant. This can be used to fine tune the output observer for for platform specific sensor errors and control loop sensitivity estimation noise.		2016-06-28 14:20:12 +10:00
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AP_NavEKF2_AirDataFusion.cpp	AP_Math: Replace the pythagorous* functions with a variadic template	2016-05-10 11:41:26 -03:00
AP_NavEKF2_Buffer.h	AP_NavEKF2: Fix typos	2016-05-13 19:20:06 -03:00
AP_NavEKF2_Control.cpp	AP_NavEKF2: Improve ground based magnetic anomaly protection for copter	2016-06-28 14:20:12 +10:00
AP_NavEKF2_core.cpp	AP_NavEKF2: Improve tracking accuracy of output predictor	2016-06-28 14:20:12 +10:00
AP_NavEKF2_core.h	AP_NavEKF2: Improve tracking accuracy of output predictor	2016-06-28 14:20:12 +10:00
AP_NavEKF2_MagFusion.cpp	AP_NavEKF2: Add tuning parameters for magentic yaw fusion	2016-06-28 14:20:12 +10:00
AP_NavEKF2_Measurements.cpp	AP_NavEKF2: Ensure corrected IMU data used by EKF	2016-06-28 14:20:12 +10:00
AP_NavEKF2_OptFlowFusion.cpp	AP_NavEKF2: Improve numerical error protection in optical flow fusion	2016-05-21 15:13:51 +10:00
AP_NavEKF2_Outputs.cpp	AP_NavEKF2: Improve ground based magnetic anomaly protection for copter	2016-06-28 14:20:12 +10:00
AP_NavEKF2_PosVelFusion.cpp	AP_NavEKF2: add height constraint during takeoff	2016-06-28 14:20:11 +10:00
AP_NavEKF2_VehicleStatus.cpp	AP_NavEKF2: Improve ground based magnetic anomaly protection for copter	2016-06-28 14:20:12 +10:00
AP_NavEKF2.cpp	AP_NavEKF2: Improve tracking accuracy of output predictor	2016-06-28 14:20:12 +10:00
AP_NavEKF2.h	AP_NavEKF2: Improve tracking accuracy of output predictor	2016-06-28 14:20:12 +10:00
AP_NavEKF_GyroBias.cpp	AP_NavEKF2: use common header for optimisation level and irq disable	2015-10-20 15:21:40 +11:00