ardupilot/libraries/AP_NavEKF
Paul Riseborough d3f83e8ec6 AP_NavEKF: Improve gyro bias learning rate for plane and rover
This patch increases initial gyro bias uncertainty and plane and rover specific process noise to improve the rate of gyro bias learning.
This reduces the likelihood of a navigation failure due to rapid temperature changes in the inertial sensors causing rapid changes in zero rate offset.

The increase in process noise cannot be applied to Copter due to different numerical stability limits arising from the faster update rate.
2015-06-03 11:46:17 +10:00
..
Models AP_NavEKF: rename file to remove spaces 2015-05-23 17:14:52 +10:00
AP_NavEKF.cpp AP_NavEKF: Improve gyro bias learning rate for plane and rover 2015-06-03 11:46:17 +10:00
AP_NavEKF.h AP_NavEKF: Enforce alignment of realigned earth mag field with declination 2015-05-19 20:35:52 +10:00
AP_Nav_Common.h AP_NavEKF: added using_gps status bit 2015-05-17 21:24:57 +10:00
AP_SmallEKF.cpp AP_NavEKF: fixed build warnings 2015-05-30 22:51:30 +10:00
AP_SmallEKF.h AP_SmallEKF: add function to report if the EKF is stable 2015-04-21 21:45:29 +09:00