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remove canonicalize and adapt comments
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@ -124,7 +124,7 @@ if(CMAKE_SOURCE_DIR STREQUAL PROJECT_SOURCE_DIR)
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include(ExternalProject)
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ExternalProject_Add(matrix
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GIT_REPOSITORY "https://github.com/PX4/Matrix.git"
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GIT_TAG 84b3da227cda0b66a2c8ebaa99aeddedf8858b02
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GIT_TAG 6b0777d815cd64902eb0575d56ec52f53aebb4a0
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UPDATE_COMMAND ""
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PATCH_COMMAND ""
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CONFIGURE_COMMAND ""
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@ -1593,10 +1593,9 @@ void Ekf::setControlEVHeight()
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// and calculate a rotation matrix which rotates EV measurements into the EKF's navigation frame
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void Ekf::calcExtVisRotMat()
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{
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// calculate the quaternion delta between the EV and EKF reference frames at the EKF fusion time horizon
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// Calculate the quaternion delta that rotates from the EV to the EKF reference frame at the EKF fusion time horizon.
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Quatf q_error = _state.quat_nominal * _ev_sample_delayed.quat.inversed();
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q_error.normalize();
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q_error.canonicalize();
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// convert to a delta angle and apply a spike and low pass filter
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Vector3f rot_vec = q_error.to_axis_angle();
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@ -1623,9 +1622,7 @@ void Ekf::calcExtVisRotMat()
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// convert filtered vector to a quaternion and then to a rotation matrix
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q_error.from_axis_angle(_ev_rot_vec_filt);
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q_error.normalize();
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q_error.canonicalize();
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_ev_rot_mat = Dcmf(q_error); // rotation from EV reference to EKF reference
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_ev_rot_mat = quat_to_invrotmat(q_error); // rotation from EV reference to EKF reference
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}
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@ -1633,7 +1630,7 @@ void Ekf::calcExtVisRotMat()
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// and update the rotation matrix which rotates EV measurements into the EKF's navigation frame
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void Ekf::resetExtVisRotMat()
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{
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// calculate the quaternion delta between the EV and EKF reference frames at the EKF fusion time horizon
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// Calculate the quaternion delta that rotates from the EV to the EKF reference frame at the EKF fusion time horizon.
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Quatf q_error = _state.quat_nominal * _ev_sample_delayed.quat.inversed();
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q_error.normalize();
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@ -1650,7 +1647,7 @@ void Ekf::resetExtVisRotMat()
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}
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// reset the rotation matrix
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_ev_rot_mat = Dcmf(q_error); // rotation from EV reference to EKF reference
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_ev_rot_mat = quat_to_invrotmat(q_error); // rotation from EV reference to EKF reference
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}
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// return the quaternions for the rotation from External Vision system reference frame to the EKF reference frame
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