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 
00031 namespace hector_pose_estimation {
00032 
00033 HeadingModel::HeadingModel()
00034   : MeasurementModel(MeasurementDimension)
00035 {
00036   parameters().add("stddev", stddev_, 10.0*M_PI/180.0);
00037 }
00038 
00039 bool HeadingModel::init()
00040 {
00041   NoiseCovariance noise = 0.0;
00042   noise(1,1) = pow(stddev_, 2);
00043   this->AdditiveNoiseSigmaSet(noise);
00044   return true;
00045 }
00046 
00047 HeadingModel::~HeadingModel() {}
00048 
00049 bool HeadingModel::applyStatusMask(const SystemStatus &status) const {
00050   if (status & STATE_YAW) return false;
00051   return true;
00052 }
00053 
00054 SystemStatus HeadingModel::getStatusFlags() const {
00055   return STATE_YAW;
00056 }
00057 
00058 ColumnVector HeadingModel::ExpectedValueGet() const {
00059   const double qw = x_(QUATERNION_W);
00060   const double qx = x_(QUATERNION_X);
00061   const double qy = x_(QUATERNION_Y);
00062   const double qz = x_(QUATERNION_Z);
00063 
00064   y_(1) = atan2(2*(qx*qy + qw*qz), qw*qw + qx*qx - qy*qy - qz*qz);
00065 
00066   return y_;
00067 }
00068 
00069 Matrix HeadingModel::dfGet(unsigned int i) const {
00070   if (i != 0) return Matrix();
00071 
00072   const double qw = x_(QUATERNION_W);
00073   const double qx = x_(QUATERNION_X);
00074   const double qy = x_(QUATERNION_Y);
00075   const double qz = x_(QUATERNION_Z);
00076   const double t1 = qw*qw + qx*qx - qy*qy - qz*qz;
00077   const double t2 = 2*(qx*qy + qw*qz);
00078   const double t3 = 1.0 / (t1*t1 + t2*t2);
00079 
00080   C_(1,QUATERNION_W) = 2.0 * t3 * (qz * t1 - qw * t2);
00081   C_(1,QUATERNION_X) = 2.0 * t3 * (qy * t1 - qx * t2);
00082   C_(1,QUATERNION_Y) = 2.0 * t3 * (qx * t1 + qy * t2);
00083   C_(1,QUATERNION_Z) = 2.0 * t3 * (qw * t1 + qz * t2);
00084 
00085   return C_;
00086 }
00087 
00088 } // namespace hector_pose_estimation
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hector_pose_estimation_core
Author(s): Johannes Meyer
autogenerated on Mon Jul 15 2013 16:48:43