Paul Riseborough 9eef97d108 AP_NavEKF2: use consistent parameter naming ... M_NSE is a measurement noise P_NSE is a observation noise I_GATE is an innovation gate This also ensures the new parameter values required to use the EKF2 will be enforced.		2016-05-25 12:06:04 +10:00
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AP_NavEKF2.cpp	AP_NavEKF2: use consistent parameter naming	2016-05-25 12:06:04 +10:00
AP_NavEKF2.h	AP_NavEKF2: extend fusion fault reporting coverage	2016-05-21 15:13:50 +10:00
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_NavEKF: remove unwanted co-variance reset	2016-05-21 15:13:53 +10:00
AP_NavEKF2_MagFusion.cpp	AP_NavEKF2: fix bug preventing in-flight alignment	2016-05-21 15:13:53 +10:00
AP_NavEKF2_Measurements.cpp	AP_NavEKF2: Remove duplicate transition into GPS aiding	2016-05-21 15:13:52 +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: Fix misleading pre-flight status reporting	2016-05-21 15:13:53 +10:00
AP_NavEKF2_PosVelFusion.cpp	AP_NavEKF2: Reset co-variance values when doing a pos,vel,hgt reset	2016-05-21 15:13:52 +10:00
AP_NavEKF2_VehicleStatus.cpp	AP_NavEKF2: Allow immediate use of GPS in-flight for plane without compass	2016-05-21 15:13:52 +10:00
AP_NavEKF2_core.cpp	AP_NavEKF2: reduce effect of acceleration on non-GPS mode attitude	2016-05-21 15:13:52 +10:00
AP_NavEKF2_core.h	AP_NavEKF2: fix comment	2016-05-21 15:13:52 +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