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msg: Add innovation test data to estimator status

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Paul Riseborough 2016-10-05 19:49:29 +11:00 committed by Lorenz Meier
parent ad65e56f47
commit 2bda15d72b
1 changed files with 20 additions and 2 deletions
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msg/estimator_status.msg
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@ -45,5 +45,23 @@ uint16 filter_fault_flags # Bitmask to indicate EKF internal faults
# 12 - true if fusion of the North position has encountered a numerical error
# 13 - true if fusion of the East position has encountered a numerical error
# 14 - true if fusion of the Down position has encountered a numerical error
float32 pos_horiz_accuracy
float32 pos_vert_accuracy
float32 pos_horiz_accuracy # 1-Sigma estimated horizontal position accuracy relative to the estimators origin (m)
float32 pos_vert_accuracy # 1-Sigma estimated vertical position accuracy relative to the estimators origin (m)
uint16 innovation_check_flags # Bitmask to indicate pass/fail status of innovation consistency checks
# 0 - true if velocity observations have been rejected
# 1 - true if horizontal position observations have been rejected
# 2 - true if true if vertical position observations have been rejected
# 3 - true if the X magnetometer observation has been rejected
# 4 - true if the Y magnetometer observation has been rejected
# 5 - true if the Z magnetometer observation has been rejected
# 6 - true if the yaw observation has been rejected
# 7 - true if the airspeed observation has been rejected
# 8 - true if the height above ground observation has been rejected
# 9 - true if the X optical flow observation has been rejected
# 10 - true if the Y optical flow observation has been rejected
float32 mag_test_ratio # ratio of the largest magnetometer innovation component to the innovation test limit
float32 vel_test_ratio # ratio of the largest velocity innovation component to the innovation test limit
float32 pos_test_ratio # ratio of the largest horizontal position innovation component to the innovation test limit
float32 hgt_test_ratio # ratio of the vertical position innovation to the innovation test limit
float32 tas_test_ratio # ratio of the true airspeed innovation to the innovation test limit
float32 hagl_test_ratio # ratio of the height above ground innovation to the innovation test limit