ardupilot/libraries/AP_NavEKF2
Paul Riseborough 2fbd050418 AP_NavEKF2: Use blended accelerometer data
If high vibration levels cause offsets between the two, it switches to the accelerometer with lower vibration levels. The default behaviour is to use the average of both accelerometers.
2015-10-20 15:21:40 +11:00
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AP_NavEKF2_AirDataFusion.cpp AP_NavEKF2: Level processor loading between frames 2015-10-20 15:21:39 +11:00
AP_NavEKF2_Control.cpp AP_NavEKF2: Update start sequence console messages 2015-10-20 15:21:39 +11:00
AP_NavEKF2_core.cpp AP_NavEKF2: Use blended accelerometer data 2015-10-20 15:21:40 +11:00
AP_NavEKF2_core.h AP_NavEKF2: Use blended accelerometer data 2015-10-20 15:21:40 +11:00
AP_NavEKF2_MagFusion.cpp AP_NavEKF2: Update magnetometer fusion documentation 2015-10-20 15:21:39 +11:00
AP_NavEKF2_Measurements.cpp AP_NavEKF2: Use blended accelerometer data 2015-10-20 15:21:40 +11:00
AP_NavEKF2_OptFlowFusion.cpp AP_NavEKF2: Level processor loading between frames 2015-10-20 15:21:39 +11:00
AP_NavEKF2_Outputs.cpp AP_NavEKF2: Make EKF2 PosDownDerivative interface follow coding conventions 2015-10-20 15:21:37 +11:00
AP_NavEKF2_PosVelFusion.cpp AP_NavEKF2: Level processor loading between frames 2015-10-20 15:21:39 +11:00
AP_NavEKF2_VehicleStatus.cpp AP_NavEKF2: Fix in-air logic bug 2015-10-20 15:21:38 +11:00
AP_NavEKF2.cpp AP_NavEKF2: Improve timing accuracy 2015-10-20 15:21:39 +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: Miscellaneous tuning changes 2015-10-20 15:21:37 +11:00