qtrocket/model/RocketModel.h
Travis Hunter e6bf1fea9b
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Revert "Merge pull request #20 from cthunter01/propagator"
This reverts commit 6280d9fb0184275843a8f4406c7293e41e65a639, reversing
changes made to 3c9c8b8c6a2b2e7430ff09efdc2cc0c1996b16ca.
2025-04-16 18:23:28 -06:00

117 lines
2.4 KiB
C++

#ifndef ROCKETMODEL_H
#define ROCKETMODEL_H
/// \cond
// C headers
// C++ headers
#include <vector>
#include <memory>
#include <string>
#include <utility> // std::move
// 3rd party headers
/// \endcond
// qtrocket headers
#include "model/Part.h"
#include "sim/Propagator.h"
#include "model/MotorModel.h"
#include "model/Propagatable.h"
// Not yet
//#include "model/Stage.h"
namespace model
{
/**
* @brief The Rocket class holds all rocket components
*
*/
class RocketModel : public Propagatable
{
public:
/**
* @brief Rocket class constructor
*/
RocketModel();
/**
* @brief Rocket class destructor
*
*/
virtual ~RocketModel() {}
/**
* @brief launch Propagates the Rocket object until termination,
* normally when altitude crosses from positive to negative
*/
void launch();
Vector3 getForces(double t) override;
Vector3 getTorques(double t) override;
/**
* @brief getMass returns current rocket mass
* @param t current simulation time
* @return mass in kg
*/
double getMass(double t) override;
/**
* @brief terminateCondition returns true or false, whether the passed-in time/state matches the terminate condition
* @param cond time/state pair
* @return true if the passed-in time/state satisfies the terminate condition
*/
bool terminateCondition(double t) override;
Matrix3 getInertiaTensor(double t) override;
/**
* @brief getThrust returns current motor thrust
* @param t current simulation time
* @return thrust in Newtons
*/
double getThrust(double t);
/**
* @brief setMotorModel
* @param motor
*/
void setMotorModel(const model::MotorModel& motor);
/**
* @brief getMotorModel
*/
MotorModel getMotorModel() { return mm; }
/**
* @brief Returns the current motor model.
* @return The current motor model
*/
//const model::MotorModel& getCurrentMotorModel() const { return mm; }
/**
* @brief setName sets the rocket name
* @param n name to set the Rocket
*/
void setName(const std::string& n) { name = n; }
double getDragCoefficient() { return 1.0; }
void setDragCoefficient(double d) { }
void setMass(double m) { }
private:
std::string name; /// Rocket name
model::MotorModel mm; /// Current Motor Model
model::Part topPart;
};
} // namespace model
#endif // ROCKETMODEL_H