ardupilot/libraries/AP_NavEKF
Paul Riseborough 44f42fe72d AP_NavEK: Reduce settling time after start-up disturbance
Now that we are using  a consistent 50Hz minimum update rate for the covariance prediction we do not need a different initial gyro bias uncertainty for plane and copter to maintain filter stability margins.
The default value of 0.1 rad/s was too high and gave excessive settling time of the filter attitude after startup.
The initial attitude uncertainty has been increased to allow for some movement during startup.
2015-10-22 16:23:14 +11:00
..
Models AP_NavEKF: rename file to remove spaces 2015-05-23 17:14:52 +10:00
AP_Nav_Common.h AP_NavEKF: Add missing GPs check report 2015-10-10 21:22:49 +09:00
AP_NavEKF.cpp AP_NavEK: Reduce settling time after start-up disturbance 2015-10-22 16:23:14 +11:00
AP_NavEKF.h NavEKF: use new perf counter API 2015-10-20 18:16:15 +11:00
AP_SmallEKF.cpp AP_NavEKF: use compass get_{field,offsets}() functions 2015-10-15 19:56:03 +09:00
AP_SmallEKF.h AP_NavEKF: standardize inclusion of libaries headers 2015-08-11 16:38:20 +10:00