00001 //================================================================================================= 00002 // Copyright (c) 2012, 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_QUADROTOR_MODEL_QUADROTOR_PROPULSION_H 00030 #define HECTOR_QUADROTOR_MODEL_QUADROTOR_PROPULSION_H 00031 00032 #include <hector_uav_msgs/Supply.h> 00033 #include <hector_uav_msgs/MotorStatus.h> 00034 #include <hector_uav_msgs/MotorPWM.h> 00035 #include <geometry_msgs/Twist.h> 00036 #include <geometry_msgs/Wrench.h> 00037 00038 #include <ros/time.h> 00039 #include <ros/forwards.h> 00040 00041 #include <queue> 00042 00043 #include <boost/thread/mutex.hpp> 00044 #include <boost/thread/condition.hpp> 00045 00046 namespace hector_quadrotor_model 00047 { 00048 00049 class QuadrotorPropulsion 00050 { 00051 public: 00052 QuadrotorPropulsion(); 00053 ~QuadrotorPropulsion(); 00054 00055 void configure(const std::string& ns = "~"); 00056 void reset(); 00057 void update(double dt); 00058 00059 void engage(); 00060 void shutdown(); 00061 00062 void setTwist(const geometry_msgs::Twist& twist); 00063 void setVoltage(const hector_uav_msgs::MotorPWM& command); 00064 00065 const geometry_msgs::Wrench& getWrench() const { return wrench_; } 00066 const hector_uav_msgs::Supply& getSupply() const { return supply_; } 00067 const hector_uav_msgs::MotorStatus& getMotorStatus() const { return motor_status_; } 00068 00069 void addVoltageToQueue(const hector_uav_msgs::MotorPWMConstPtr& command); 00070 bool processQueue(const ros::Time& timestamp, const ros::Duration& tolerance = ros::Duration(), const ros::Duration& delay = ros::Duration(), const ros::WallDuration &wait = ros::WallDuration(), ros::CallbackQueue *callback_queue = 0); 00071 00072 void f(const double xin[4], const double uin[10], double dt, double y[14], double xpred[4]) const; 00073 00074 void setInitialSupplyVoltage(double voltage) { initial_voltage_ = voltage; } 00075 00076 private: 00077 geometry_msgs::Wrench wrench_; 00078 hector_uav_msgs::Supply supply_; 00079 hector_uav_msgs::MotorStatus motor_status_; 00080 ros::Time last_command_time_; 00081 00082 double initial_voltage_; 00083 00084 std::queue<hector_uav_msgs::MotorPWMConstPtr> command_queue_; 00085 boost::mutex command_queue_mutex_; 00086 boost::condition command_condition_; 00087 00088 boost::mutex mutex_; 00089 00090 class PropulsionModel; 00091 PropulsionModel *propulsion_model_; 00092 }; 00093 00094 } 00095 00096 #endif // HECTOR_QUADROTOR_MODEL_QUADROTOR_PROPULSION_H