QuaternionBaseAddons.h
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00001 //=================================================================================================
00002 // Copyright (c) 2014, Johannes Meyer and contributors, Technische Universitat Darmstadt
00003 // All rights reserved.
00004 
00005 // Redistribution and use in source and binary forms, with or without
00006 // modification, are permitted provided that the following conditions are met:
00007 //     * Redistributions of source code must retain the above copyright
00008 //       notice, this list of conditions and the following disclaimer.
00009 //     * Redistributions in binary form must reproduce the above copyright
00010 //       notice, this list of conditions and the following disclaimer in the
00011 //       documentation and/or other materials provided with the distribution.
00012 //     * Neither the name of the Flight Systems and Automatic Control group,
00013 //       TU Darmstadt, nor the names of its contributors may be used to
00014 //       endorse or promote products derived from this software without
00015 //       specific prior written permission.
00016 
00017 // THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS" AND
00018 // ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE IMPLIED
00019 // WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE ARE
00020 // DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT HOLDER BE LIABLE FOR ANY
00021 // DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES
00022 // (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
00023 // LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND
00024 // ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT
00025 // (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE OF THIS
00026 // SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE.
00027 //=================================================================================================
00028 
00029 #ifndef HECTOR_POSE_ESTIMATION_EIGEN_QUATERNIONBASE_PLUGIN
00030 #define HECTOR_POSE_ESTIMATION_EIGEN_QUATERNIONBASE_PLUGIN
00031 
00032 #ifndef EIGEN_QUATERNIONBASE_PLUGIN
00033   #define EIGEN_QUATERNIONBASE_PLUGIN <hector_pose_estimation/Eigen/QuaternionBaseAddons.h>
00034 #endif
00035 
00036 #else  // HECTOR_POSE_ESTIMATION_EIGEN_QUATERNIONBASE_PLUGIN
00037 
00038 template <typename OtherDerived>
00039 Derived &fromRotationVector(const MatrixBase<OtherDerived> &rotation_vector)
00040 {
00041   eigen_assert(rotation_vector.size() == 3);
00042 
00043   const double angle = rotation_vector.norm();
00044   double sin_angle_2, cos_angle_2;
00045   ::sincos(angle / 2., &sin_angle_2, &cos_angle_2);
00046   double sin_angle_norm_2 = 0.5;
00047   if (angle > NumTraits<double>::dummy_precision()) sin_angle_norm_2 = sin_angle_2 / angle;
00048 
00049   w() = cos_angle_2;
00050   vec() = rotation_vector * sin_angle_norm_2;
00051 
00052   return derived();
00053 }
00054 
00055 Vector3 toRotationVector() const
00056 {
00057   eigen_assert(squaredNorm() == 1.0);
00058   Scalar vector_norm = vec().norm();
00059   if (vector_norm <= NumTraits<Scalar>::dummy_precision())
00060     return vec() * Scalar(2.);
00061   else
00062     return vec() / vector_norm * ::acos(w()) * Scalar(2.);
00063 }
00064 
00065 #endif // HECTOR_POSE_ESTIMATION_EIGEN_QUATERNIONBASE_PLUGIN


hector_pose_estimation_core
Author(s): Johannes Meyer
autogenerated on Mon Aug 22 2016 03:53:11