ardupilot/libraries/AP_NavEKF
Paul Riseborough 19d1b3b813 AP_NavEKF: Update EKF origin height whilst disarmed
This patch causes the EKF to update the height of its origin each time it receives a valid GPs message whislt disarmed.
The resultant EKF origin height represents the height of the zero baro alt datum relative to the GPS height datum.
2015-04-03 15:15:08 -07:00
..
AP_NavEKF.cpp AP_NavEKF: Update EKF origin height whilst disarmed 2015-04-03 15:15:08 -07:00
AP_NavEKF.h AP_NavEKF: Add second stage alignment of yaw and earth field states 2015-04-03 15:15:08 -07:00
AP_Nav_Common.h AP_NavEKF: add pred_horiz_pos flags to filter status 2015-01-09 10:51:23 +11:00
AP_SmallEKF.cpp AP_NavEKF: use compass->last_update_usec() 2015-03-14 12:31:39 +11:00
AP_SmallEKF.h AP_NavEKF: Publish small EKF quaternion and gyro bias outputs 2015-02-03 09:49:16 +11:00