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PX4-Autopilot/EKF
History
Paul Riseborough ffe1d30864 EKF: Set covariances to zero for un-used states
2016-02-16 11:08:30 +11:00
..
tests
added tests for EKF ringbuffer
2015-12-07 22:41:11 +01:00
common.h
EKF: Add control mode for wind state estimation
2016-02-16 11:08:30 +11:00
control.cpp
EKF: Enable control mode transitions to be detected
2016-02-16 11:08:30 +11:00
covariance.cpp
EKF: Set covariances to zero for un-used states
2016-02-16 11:08:30 +11:00
ekf_helper.cpp
EKF: Reset covariance matrix when doing a yaw and magnetic field reset
2016-02-14 22:01:53 +01:00
ekf.cpp
EKF: Split tilt and yaw align
2016-02-14 22:01:53 +01:00
ekf.h
EKF: Enable control mode transitions to be detected
2016-02-16 11:08:30 +11:00
estimator_interface.cpp
-added comments
2016-02-14 09:49:26 +01:00
estimator_interface.h
EKF: Publish the magnetic declination we wish to save for next startup
2016-02-14 22:01:53 +01:00
gps_checks.cpp
EKF: Add function to calculate the magnetic declination to use
2016-02-14 22:01:53 +01:00
mag_fusion.cpp
EKF: Set Kaman gains to zero for un-used states
2016-02-16 11:08:30 +11:00
RingBuffer.h
-added comments
2016-02-14 09:49:26 +01:00
vel_pos_fusion.cpp
EKF: Set Kaman gains to zero for un-used states
2016-02-16 11:08:30 +11:00
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