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/imu_input.h> 00034 #include <hector_pose_estimation/system/imu_model.h> 00035 00036 namespace hector_pose_estimation { 00037 00038 class GenericQuaternionSystemModel; 00039 00040 namespace traits { 00041 template <> struct Input<GenericQuaternionSystemModel> { 00042 enum { Dimension = ImuInput::Dimension }; 00043 typedef ImuInput Type; 00044 typedef ImuInput::Vector Vector; 00045 typedef ImuInput::Variance Variance; 00046 }; 00047 } // namespace traits 00048 00049 class GenericQuaternionSystemModel : public TimeContinuousSystemModel_<GenericQuaternionSystemModel> 00050 { 00051 public: 00052 GenericQuaternionSystemModel(); 00053 virtual ~GenericQuaternionSystemModel(); 00054 00055 virtual bool init(PoseEstimation& estimator, State& state); 00056 00057 virtual void getPrior(State &state); 00058 00059 virtual bool prepareUpdate(State& state, double dt); 00060 virtual SystemStatus getStatusFlags(const State& state); 00061 00062 using TimeContinuousSystemModel_<GenericQuaternionSystemModel>::getDerivative; 00063 virtual void getDerivative(StateVector& x_dot, const State& state); 00064 using TimeContinuousSystemModel_<GenericQuaternionSystemModel>::getSystemNoise; 00065 virtual void getSystemNoise(NoiseVariance& Q, const State& state, bool init); 00066 using TimeContinuousSystemModel_<GenericQuaternionSystemModel>::getStateJacobian; 00067 virtual void getStateJacobian(SystemMatrix& A, const State& state, bool init); 00068 using TimeContinuousSystemModel_<GenericQuaternionSystemModel>::getInputJacobian; 00069 virtual void getInputJacobian(InputMatrix& B, const State& state, bool init); 00070 00071 void setGravity(double gravity) { gravity_ = gravity; } 00072 double getGravity() const { return gravity_; } 00073 00074 protected: 00075 AliasT<double> gravity_; 00076 AliasT<double> rate_stddev_; 00077 AliasT<double> acceleration_stddev_; 00078 double angular_acceleration_stddev_; 00079 double velocity_stddev_; 00080 00081 boost::shared_ptr<ImuInput> imu_; 00082 boost::shared_ptr<Gyro> gyro_; 00083 boost::shared_ptr<Accelerometer> accelerometer_; 00084 00085 ColumnVector_<3> rate; 00086 ColumnVector_<3> acceleration; 00087 State::RotationMatrix R; 00088 }; 00089 00090 extern template class System_<GenericQuaternionSystemModel>; 00091 00092 } // namespace hector_pose_estimation 00093 00094 #endif // HECTOR_POSE_ESTIMATION_GENERIC_QUATERNION_SYSTEM_MODEL_H