heading.cpp
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00001 //=================================================================================================
00002 // Copyright (c) 2011, Johannes Meyer, TU 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 #include <hector_pose_estimation/measurements/heading.h>
00030 #include <hector_pose_estimation/filter/set_filter.h>
00031 
00032 namespace hector_pose_estimation {
00033 
00034 template class Measurement_<HeadingModel>;
00035 
00036 HeadingModel::HeadingModel()
00037 {
00038   parameters().add("stddev", stddev_, 10.0*M_PI/180.0);
00039 }
00040 
00041 HeadingModel::~HeadingModel() {}
00042 
00043 void HeadingModel::getMeasurementNoise(NoiseVariance& R, const State&, bool init)
00044 {
00045   if (init) {
00046     R(0,0) = pow(stddev_, 2);
00047   }
00048 }
00049 
00050 void HeadingModel::getExpectedValue(MeasurementVector& y_pred, const State& state)
00051 {
00052   State::ConstOrientationType q(state.getOrientation());
00053   y_pred(0) = atan2(2*(q.x()*q.y() + q.w()*q.z()), q.w()*q.w() + q.x()*q.x() - q.y()*q.y() - q.z()*q.z());
00054 }
00055 
00056 void HeadingModel::getStateJacobian(MeasurementMatrix& C, const State& state, bool)
00057 {
00058   State::ConstOrientationType q(state.getOrientation());
00059   const double t1 = q.w()*q.w() + q.x()*q.x() - q.y()*q.y() - q.z()*q.z();
00060   const double t2 = 2*(q.x()*q.y() + q.w()*q.z());
00061   const double t3 = 1.0 / (t1*t1 + t2*t2);
00062 
00063   if (state.getOrientationIndex() >= 0) {
00064     C(0,State::QUATERNION_W) = 2.0 * t3 * (q.z() * t1 - q.w() * t2);
00065     C(0,State::QUATERNION_X) = 2.0 * t3 * (q.y() * t1 - q.x() * t2);
00066     C(0,State::QUATERNION_Y) = 2.0 * t3 * (q.x() * t1 + q.y() * t2);
00067     C(0,State::QUATERNION_Z) = 2.0 * t3 * (q.w() * t1 + q.z() * t2);
00068   }
00069 }
00070 
00071 void HeadingModel::limitError(MeasurementVector &error) {
00072   error(0) = remainder(error(0), 2 * M_PI);
00073 }
00074 
00075 } // namespace hector_pose_estimation


hector_pose_estimation_core
Author(s): Johannes Meyer
autogenerated on Mon Oct 6 2014 00:24:16