generic_quaternion_system_model.h
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00001 //=================================================================================================
00002 // Copyright (c) 2011, Johannes Meyer and Martin Nowara, 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_GENERIC_QUATERNION_SYSTEM_MODEL_H
00030 #define HECTOR_POSE_ESTIMATION_GENERIC_QUATERNION_SYSTEM_MODEL_H
00031 
00032 #include <hector_pose_estimation/system_model.h>
00033 #include <hector_pose_estimation/system.h>
00034 
00035 #include <hector_pose_estimation/system/imu_input.h>
00036 #include <hector_pose_estimation/system/imu_model.h>
00037 
00038 namespace hector_pose_estimation {
00039 
00040 class GenericQuaternionSystemModel;
00041 
00042 //namespace traits {
00043 //  template <> struct Input<GenericQuaternionSystemModel> {
00044 //    enum { Dimension = ImuInput::Dimension };
00045 //    typedef ImuInput Type;
00046 //    typedef ImuInput::Vector Vector;
00047 //    typedef ImuInput::Variance Variance;
00048 //  };
00049 //} // namespace traits
00050 
00051 class GenericQuaternionSystemModel : public TimeContinuousSystemModel_<GenericQuaternionSystemModel>
00052 {
00053 public:
00054   EIGEN_MAKE_ALIGNED_OPERATOR_NEW
00055 
00056   GenericQuaternionSystemModel();
00057   virtual ~GenericQuaternionSystemModel();
00058 
00059   virtual bool init(PoseEstimation& estimator, System &system, State& state);
00060 
00061   virtual void getPrior(State &state);
00062 
00063   virtual SystemStatus getStatusFlags(const State& state);
00064 
00065   bool prepareUpdate(State& state, double dt);
00066 
00067   using TimeContinuousSystemModel_<GenericQuaternionSystemModel>::getDerivative;
00068   virtual void getDerivative(StateVector& x_dot, const State& state);
00069   using TimeContinuousSystemModel_<GenericQuaternionSystemModel>::getSystemNoise;
00070   virtual void getSystemNoise(NoiseVariance& Q, const State& state, bool init = true);
00071   using TimeContinuousSystemModel_<GenericQuaternionSystemModel>::getStateJacobian;
00072   virtual void getStateJacobian(SystemMatrix& A, const State& state, bool init = true);
00073 
00074 //  void setGravity(double gravity) { gravity_ = gravity; }
00075 //  double getGravity() const { return gravity_; }
00076 
00077 protected:
00078   AliasT<double> gravity_;
00079   double rate_stddev_;
00080   double acceleration_stddev_;
00081   double angular_acceleration_stddev_;
00082   double velocity_stddev_;
00083 
00084   boost::shared_ptr<ImuInput> imu_;
00085   boost::shared_ptr<Gyro> gyro_;
00086   boost::shared_ptr<Accelerometer> accelerometer_;
00087 
00088   ColumnVector3 rate_nav_;
00089   ColumnVector3 acceleration_nav_;
00090 //  State::Covariance Q_;
00091 
00092   typedef Input_<3> TorqueInput;
00093   TorqueInput::Ptr torque_input_;
00094   typedef Input_<3> RateInput;
00095   RateInput::Ptr rate_input_;
00096   typedef Input_<3> ForceInput;
00097   ForceInput::Ptr force_input_;
00098 };
00099 
00100 extern template class System_<GenericQuaternionSystemModel>;
00101 
00102 } // namespace hector_pose_estimation
00103 
00104 #endif // HECTOR_POSE_ESTIMATION_GENERIC_QUATERNION_SYSTEM_MODEL_H


hector_pose_estimation_core
Author(s): Johannes Meyer
autogenerated on Fri Aug 28 2015 10:59:54