ardupilot/libraries/AP_NavEKF2
Paul Riseborough 225b81baf4 AP_NavEKF2: Prevent users breaking filter by setting excessive time delays
If time deelays greater than the IMU buffer length are used, then it is possible for measurements to be dropped.
2015-10-20 15:21:39 +11:00
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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_NavEKF2_AirDataFusion.cpp AP_NavEKF2: Update function header comments 2015-10-20 15:21:38 +11:00
AP_NavEKF2_Control.cpp AP_NavEKF2: Allow use of magnetometer learning during optical flow nav 2015-10-20 15:21:38 +11:00
AP_NavEKF2_MagFusion.cpp AP_NavEKF2: Allow use of magnetometer learning during optical flow nav 2015-10-20 15:21:38 +11:00
AP_NavEKF2_Measurements.cpp AP_NavEKF2: Prevent users breaking filter by setting excessive time delays 2015-10-20 15:21:39 +11:00
AP_NavEKF2_OptFlowFusion.cpp AP_NavEKF2: Update function header comments 2015-10-20 15:21:38 +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: Rename files and re-distribute content 2015-10-10 14:48:50 +09:00
AP_NavEKF2_VehicleStatus.cpp AP_NavEKF2: Fix in-air logic bug 2015-10-20 15:21:38 +11:00
AP_NavEKF2_core.cpp AP_NavEKF2: Prevent users breaking filter by setting excessive time delays 2015-10-20 15:21:39 +11:00
AP_NavEKF2_core.h AP_NavEKF2: Prevent users breaking filter by setting excessive time delays 2015-10-20 15:21:39 +11:00
AP_NavEKF_GyroBias.cpp AP_NavEKF2: Miscellaneous tuning changes 2015-10-20 15:21:37 +11:00