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estimator_status split out estimator_states
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@@ -62,6 +62,7 @@ set(msg_files
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esc_status.msg
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estimator_innovations.msg
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estimator_sensor_bias.msg
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estimator_states.msg
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estimator_status.msg
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follow_target.msg
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geofence_result.msg
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@@ -0,0 +1,6 @@
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uint64 timestamp # time since system start (microseconds)
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float32[24] states # Internal filter states
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uint8 n_states # Number of states effectively used
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float32[24] covariances # Diagonal Elements of Covariance Matrix
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@@ -1,14 +1,10 @@
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uint64 timestamp # time since system start (microseconds)
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float32[24] states # Internal filter states
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uint8 n_states # Number of states effectively used
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float32[3] vibe # IMU vibration metrics in the following array locations
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# 0 : Gyro delta angle coning metric = filtered length of (delta_angle x prev_delta_angle)
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# 1 : Gyro high frequency vibe = filtered length of (delta_angle - prev_delta_angle)
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# 2 : Accel high frequency vibe = filtered length of (delta_velocity - prev_delta_velocity)
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float32[24] covariances # Diagonal Elements of Covariance Matrix
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float32[3] output_tracking_error # return a vector containing the output predictor angular, velocity and position tracking error magnitudes (rad), (m/s), (m)
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uint16 gps_check_fail_flags # Bitmask to indicate status of GPS checks - see definition below
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@@ -281,6 +281,8 @@ rtps:
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id: 133
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- msg: sensor_preflight_mag
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id: 134
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- msg: estimator_states
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id: 135
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########## multi topics: begin ##########
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- msg: actuator_controls_0
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id: 150
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