106 lines
2.3 KiB
C++
106 lines
2.3 KiB
C++
#ifndef ROCKET_H
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#define ROCKET_H
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/// \cond
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// C headers
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// C++ headers
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#include <vector>
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#include <memory>
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#include <string>
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#include <utility> // std::move
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// 3rd party headers
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/// \endcond
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// qtrocket headers
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#include "sim/Propagator.h"
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#include "model/Stage.h"
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#include "model/Propagatable.h"
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namespace model
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{
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/**
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* @brief The Rocket class holds all rocket components
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*
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*/
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class Rocket : public Propagatable
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{
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public:
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/**
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* @brief Rocket class constructor
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*/
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Rocket();
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/**
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* @brief Rocket class destructor
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*
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*/
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virtual ~Rocket() {}
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/**
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* @brief launch Propagates the Rocket object until termination,
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* normally when altitude crosses from positive to negative
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*/
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void launch();
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/**
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* @brief getThrust returns current motor thrust
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* @param t current simulation time
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* @return thrust in Newtons
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*/
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double getThrust(double t) override;
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/**
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* @brief getMass returns current rocket
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* @param t current simulation time
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* @return mass in kg
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*/
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double getMass(double t) override;
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/**
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* @brief setMotorModel
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* @param motor
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*/
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void setMotorModel(const model::MotorModel& motor);
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/**
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* @brief Returns the current motor model.
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* @return The current motor model
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*/
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//const model::MotorModel& getCurrentMotorModel() const { return mm; }
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/**
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* @brief terminateCondition returns true or false, whether the passed-in time/state matches the terminate condition
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* @param cond time/state pair
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* @return true if the passed-in time/state satisfies the terminate condition
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*/
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virtual bool terminateCondition(const std::pair<double, StateData>& cond) override;
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/**
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* @brief setName sets the rocket name
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* @param n name to set the Rocket
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*/
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void setName(const std::string& n) { name = n; }
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double getDragCoefficient() override { return 1.0; }
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void setDragCoefficient(double d) override { }
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void setMass(double m) { }
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std::shared_ptr<Stage> getCurrentStage() { return currentStage; }
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private:
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std::string name; /// Rocket name
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std::vector<std::shared_ptr<Stage>> stages;
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std::shared_ptr<Stage> currentStage;
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//model::MotorModel mm; /// Current Motor Model
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};
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} // namespace model
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#endif // ROCKET_H
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