gravity.h
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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 #ifndef HECTOR_POSE_ESTIMATION_GRAVITY_H
00030 #define HECTOR_POSE_ESTIMATION_GRAVITY_H
00031 
00032 #include <hector_pose_estimation/measurement.h>
00033 
00034 namespace hector_pose_estimation {
00035 
00036 class GravityModel : public MeasurementModel_<GravityModel,3> {
00037 public:
00038   using MeasurementModel_<GravityModel,3>::MeasurementVector;
00039   using MeasurementModel_<GravityModel,3>::NoiseVariance;
00040 
00041   GravityModel();
00042   virtual ~GravityModel();
00043 
00044   virtual bool init(PoseEstimation &estimator, State &state);
00045 
00046   virtual void setGravity(double gravity) { gravity_.z() = gravity; }
00047   virtual double getGravity() const { return gravity_.z(); }
00048 
00049   virtual bool active(const State &state) { return !(state.getSystemStatus() & STATE_ROLLPITCH); }
00050   virtual SystemStatus getStatusFlags() { return STATE_PSEUDO_ROLLPITCH; }
00051 
00052   virtual void getMeasurementNoise(NoiseVariance& R, const State&, bool init);
00053   virtual void getExpectedValue(MeasurementVector& y_pred, const State& state);
00054   virtual void getStateJacobian(MeasurementMatrix& C, const State& state, bool init);
00055 
00056 protected:
00057   double stddev_;
00058   MeasurementVector gravity_;
00059 };
00060 
00061 typedef Measurement_<GravityModel> Gravity;
00062 extern template class Measurement_<GravityModel>;
00063 
00064 } // namespace hector_pose_estimation
00065 
00066 #endif // HECTOR_POSE_ESTIMATION_GRAVITY_H


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