quadrotor_propulsion.h

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//=================================================================================================
// Copyright (c) 2012-2016, Institute of Flight Systems and Automatic Control,
// Technische Universität Darmstadt.
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#ifndef HECTOR_QUADROTOR_MODEL_QUADROTOR_PROPULSION_H
#define HECTOR_QUADROTOR_MODEL_QUADROTOR_PROPULSION_H

#include <hector_uav_msgs/Supply.h>
#include <hector_uav_msgs/MotorStatus.h>
#include <hector_uav_msgs/MotorCommand.h>
#include <hector_uav_msgs/MotorPWM.h>
#include <geometry_msgs/Twist.h>
#include <geometry_msgs/Wrench.h>

#include <ros/forwards.h>
#include <ros/node_handle.h>
#include <ros/time.h>

#include <queue>

#include <boost/thread/mutex.hpp>
#include <boost/thread/condition.hpp>

namespace hector_quadrotor_model
{

class QuadrotorPropulsion
{
public:
  QuadrotorPropulsion();
  ~QuadrotorPropulsion();

  bool configure(const ros::NodeHandle &param = ros::NodeHandle("~"));
  void reset();
  void update(double dt);

  void engage();
  void shutdown();

  void setTwist(const geometry_msgs::Twist& twist);
  void setVoltage(const hector_uav_msgs::MotorPWM& command);

  const geometry_msgs::Wrench& getWrench() const { return wrench_; }
  const hector_uav_msgs::Supply& getSupply() const { return supply_; }
  const hector_uav_msgs::MotorStatus& getMotorStatus() const { return motor_status_; }

  void addCommandToQueue(const hector_uav_msgs::MotorCommandConstPtr& command);
  void addPWMToQueue(const hector_uav_msgs::MotorPWMConstPtr& pwm);
  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);

  void f(const double xin[4], const double uin[10], double dt, double y[14], double xpred[4]) const;

  void setInitialSupplyVoltage(double voltage) { initial_voltage_ = voltage; }

private:
  geometry_msgs::Wrench wrench_;
  hector_uav_msgs::Supply supply_;
  hector_uav_msgs::MotorStatus motor_status_;
  ros::Time last_command_time_;

  double initial_voltage_;

  std::queue<hector_uav_msgs::MotorPWMConstPtr> command_queue_;
  boost::mutex command_queue_mutex_;
  boost::condition command_condition_;

  boost::mutex mutex_;

  class PropulsionModel;
  PropulsionModel *propulsion_model_;
};

}

#endif // HECTOR_QUADROTOR_MODEL_QUADROTOR_PROPULSION_H