Paul Riseborough 4fdec67546 AP_NavEKF2: Publish the position and velocity state reset deltas ... Used by the control loops to compensate for step changes in position and velocity when the EKF needs to do a reset of these states.		2015-10-30 12:24:02 +09:00
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AP_NavEKF2_AirDataFusion.cpp	AP_NavEKF: prevent high rate mag data locking out other data fusion	2015-10-20 20:16:04 +11:00
AP_NavEKF2_Control.cpp	AP_NavEKF: Reduce roll/pitch disturbance when magnetic field is reset	2015-10-23 19:04:30 +11:00
AP_NavEKF2_core.cpp	AP_NavEKF2: Remove dead code	2015-10-26 08:05:15 +11:00
AP_NavEKF2_core.h	AP_NavEKF2: Publish the position and velocity state reset deltas	2015-10-30 12:24:02 +09:00
AP_NavEKF2_MagFusion.cpp	AP_NavEKF2: Reduce allowance for magnetometer timing errors	2015-10-26 08:05:15 +11:00
AP_NavEKF2_Measurements.cpp	AP_NavEKF2: Ensure consistent position and velocity fusion rates when not using GPS	2015-10-21 17:27:00 +11:00
AP_NavEKF2_OptFlowFusion.cpp	AP_NavEKF: prevent high rate mag data locking out other data fusion	2015-10-20 20:16:04 +11:00
AP_NavEKF2_Outputs.cpp	AP_NavEKF2: Publish the position and velocity state reset deltas	2015-10-30 12:24:02 +09:00
AP_NavEKF2_PosVelFusion.cpp	AP_NavEKF2: Improve handling of GPS loss and recovery for planes	2015-10-24 07:17:11 +11:00
AP_NavEKF2_VehicleStatus.cpp	AP_NavEKF2: use common header for optimisation level and irq disable	2015-10-20 15:21:40 +11:00
AP_NavEKF2.cpp	AP_NavEKF2: prevent a valgrind error on startup	2015-10-26 11:34:32 +11:00
AP_NavEKF2.h	AP_NavEKF2: Reduce effect of rounding errors on covariance prediction	2015-10-20 15:21:37 +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