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Diffstat (limited to 'src/modules/ekf_att_pos_estimator')
-rw-r--r--src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp12
1 files changed, 6 insertions, 6 deletions
diff --git a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp
index 7d3cb5396..903158129 100644
--- a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp
+++ b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp
@@ -772,14 +772,14 @@ void AttitudePositionEstimatorEKF::publishAttitude()
_att.pitch = euler(1);
_att.yaw = euler(2);
- _att.rollspeed = _ekf->angRate.x - _ekf->states[10];
- _att.pitchspeed = _ekf->angRate.y - _ekf->states[11];
- _att.yawspeed = _ekf->angRate.z - _ekf->states[12];
+ _att.rollspeed = _ekf->angRate.x - _ekf->states[10] / _ekf->dtIMU;
+ _att.pitchspeed = _ekf->angRate.y - _ekf->states[11] / _ekf->dtIMU;
+ _att.yawspeed = _ekf->angRate.z - _ekf->states[12] / _ekf->dtIMU;
// gyro offsets
- _att.rate_offsets[0] = _ekf->states[10];
- _att.rate_offsets[1] = _ekf->states[11];
- _att.rate_offsets[2] = _ekf->states[12];
+ _att.rate_offsets[0] = _ekf->states[10] / _ekf->dtIMU;
+ _att.rate_offsets[1] = _ekf->states[11] / _ekf->dtIMU;
+ _att.rate_offsets[2] = _ekf->states[12] / _ekf->dtIMU;
/* lazily publish the attitude only once available */
if (_att_pub > 0) {