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EKF: Remove use of quaternion self product operator and fix delta rotation sign error

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Paul Riseborough
2019-06-14 09:47:44 +10:00
committed by Paul Riseborough
parent ad7f7af03b
commit 0e946f25fd
1 changed files with 6 additions and 8 deletions
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EKF/ekf_helper.cpp
+6 -8
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@@ -506,17 +506,16 @@ bool Ekf::realignYawGPS()
_flt_mag_align_start_time = _imu_sample_delayed.time_us;
// calculate the amount that the quaternion has changed by
_state_reset_status.quat_change = quat_before_reset.inversed() * _state.quat_nominal;
_state_reset_status.quat_change = _state.quat_nominal * quat_before_reset.inversed();
// add the reset amount to the output observer buffered data
// Note q1 *= q2 is equivalent to q1 = q1 * q2
for (uint8_t i = 0; i < _output_buffer.get_length(); i++) {
_output_buffer[i].quat_nominal *= _state_reset_status.quat_change;
_output_buffer[i].quat_nominal = _state_reset_status.quat_change * _output_buffer[i].quat_nominal;
}
// apply the change in attitude quaternion to our newest quaternion estimate
// which was already taken out from the output buffer
_output_new.quat_nominal = _output_new.quat_nominal * _state_reset_status.quat_change;
_output_new.quat_nominal = _state_reset_status.quat_change * _output_new.quat_nominal;
// capture the reset event
_state_reset_status.quat_counter++;
@@ -718,7 +717,7 @@ bool Ekf::resetMagHeading(Vector3f &mag_init, bool increase_yaw_var, bool update
_flt_mag_align_start_time = _imu_sample_delayed.time_us;
// calculate the amount that the quaternion has changed by
Quatf q_error = quat_before_reset.inversed() * quat_after_reset;
Quatf q_error = quat_after_reset * quat_before_reset.inversed();
q_error.normalize();
// update quaternion states
@@ -750,13 +749,12 @@ bool Ekf::resetMagHeading(Vector3f &mag_init, bool increase_yaw_var, bool update
if (update_buffer) {
// add the reset amount to the output observer buffered data
for (uint8_t i = 0; i < _output_buffer.get_length(); i++) {
// Note q1 *= q2 is equivalent to q1 = q1 * q2
_output_buffer[i].quat_nominal *= _state_reset_status.quat_change;
_output_buffer[i].quat_nominal = _state_reset_status.quat_change * _output_buffer[i].quat_nominal;
}
// apply the change in attitude quaternion to our newest quaternion estimate
// which was already taken out from the output buffer
_output_new.quat_nominal = _output_new.quat_nominal * _state_reset_status.quat_change;
_output_new.quat_nominal = _state_reset_status.quat_change * _output_new.quat_nominal;
}
// capture the reset event