WsfRocketOrbitalManeuvering::Rocket Class Reference

#include <WsfRocketOrbitalManeuvering.hpp>

Public Member Functions
	Rocket ()
	Rocket (const Rocket &aSrc)
Rocket &	operator= (const Rocket &)=delete
	~Rocket ()=default
bool	Initialize ()
bool	ProcessInput (UtInput &aInput)
double	Thrust (double aDuration, double &aDeltaV)
double	GetDuration (double aDeltaV) const
double	GetDeltaV (double aDuration) const
double	GetAvailableDeltaV () const
	Return the total delta-v available for the entire multi-stage rocket.
double	GetAvailableDuration () const
double	GetTotalMass () const
	Return the total mass of the rocket, including all stages.
double	GetFuelMass () const
	Return the fuel mass, considered to be the fuel for this stage only.
double	GetEmptyMass () const
double	GetPayloadMass () const
	Return the payload mass, which is the total mass of all subsequent stages, if any.
bool	PerformStagingOperation ()
	Perform a staging event for the rocket. If no other stages are present, false is returned.

Constructor & Destructor Documentation

Rocket() [1/2]

WsfRocketOrbitalManeuvering::Rocket::Rocket

(

)

Referenced by operator=(), and Rocket().

Rocket() [2/2]

WsfRocketOrbitalManeuvering::Rocket::Rocket

(

const Rocket &

aSrc

)

References begin(), and Rocket().

~Rocket()

WsfRocketOrbitalManeuvering::Rocket::~Rocket ( )

default

References GetAvailableDeltaV(), GetAvailableDuration(), GetDeltaV(), GetDuration(), GetEmptyMass(), GetFuelMass(), GetPayloadMass(), GetTotalMass(), Initialize(), PerformStagingOperation(), ProcessInput(), and Thrust().

Member Function Documentation

GetAvailableDeltaV()

double WsfRocketOrbitalManeuvering::Rocket::GetAvailableDeltaV

(

)

const

Return the total delta-v available for the entire multi-stage rocket.

References WsfRocketOrbitalManeuvering::GetTotalMass().

Referenced by ~Rocket().

GetAvailableDuration()

double WsfRocketOrbitalManeuvering::Rocket::GetAvailableDuration

(

)

const

Referenced by ~Rocket().

GetDeltaV()

double WsfRocketOrbitalManeuvering::Rocket::GetDeltaV

(

double

aDuration

)

const

Return the delta-v necessary to execute a maneuver with the specified duration, given the current mass properties of the rocket.

Parameters

aDuration

The duration for which the rocket will thrust.

Returns

The delta-v that would be expended to complete the maneuver. If the rocket does not have sufficient fuel to thrust for the given duration of the maneuver, WsfOrbitalManeuvering::cINFINITE_DELTA_V is returned.

References WsfOrbitalManeuvering::cINFINITE_DELTA_V, and WsfRocketOrbitalManeuvering::GetTotalMass().

Referenced by ~Rocket().

GetDuration()

double WsfRocketOrbitalManeuvering::Rocket::GetDuration

(

double

aDeltaV

)

const

Return how long it will take to execute a maneuver with the specified delta-V, given the current mass properties of the rocket.

Parameters

aDeltaV

The delta-V to expend in the maneuver.

Returns

The time necessary to complete the maneuver. If the rocket does not have sufficient delta-v to complete the maneuver, WsfOrbitalManeuvering::cINFINITE_DURATION is returned.

References WsfOrbitalManeuvering::cINFINITE_DURATION, and WsfRocketOrbitalManeuvering::GetTotalMass().

Referenced by ~Rocket().

GetEmptyMass()

double WsfRocketOrbitalManeuvering::Rocket::GetEmptyMass

(

)

const

Return the empty mass, considered to be the total mass of this stage minus the fuel mass for this stage.

Note

This definition is consistent with the definition in WsfPlatform, such that the total mass must equal the empty mass + fuel mass + payload mass.

Referenced by ~Rocket().

GetFuelMass()

double WsfRocketOrbitalManeuvering::Rocket::GetFuelMass

(

)

const

Return the fuel mass, considered to be the fuel for this stage only.

Referenced by ~Rocket().

GetPayloadMass()

double WsfRocketOrbitalManeuvering::Rocket::GetPayloadMass

(

)

const

Return the payload mass, which is the total mass of all subsequent stages, if any.

References WsfRocketOrbitalManeuvering::GetTotalMass().

Referenced by ~Rocket().

GetTotalMass()

double WsfRocketOrbitalManeuvering::Rocket::GetTotalMass

(

)

const

Return the total mass of the rocket, including all stages.

Referenced by ~Rocket().

Initialize()

bool WsfRocketOrbitalManeuvering::Rocket::Initialize

(

)

References ok.

Referenced by ~Rocket().

operator=()

Rocket & WsfRocketOrbitalManeuvering::Rocket::operator= ( const Rocket & )

delete

References Rocket().

PerformStagingOperation()

bool WsfRocketOrbitalManeuvering::Rocket::PerformStagingOperation

(

)

Perform a staging event for the rocket. If no other stages are present, false is returned.

Referenced by ~Rocket().

ProcessInput()

bool WsfRocketOrbitalManeuvering::Rocket::ProcessInput

(

UtInput &

aInput

)

References WsfRocketOrbitalManeuvering::Stage::ProcessInput().

Referenced by ~Rocket().

Thrust()

double WsfRocketOrbitalManeuvering::Rocket::Thrust	(	double	aDuration,
		double &	aDeltaV )

Expend fuel / Delta-V for the specified duration. If the current stage would expend its fuel, and automatic staging is enabled, the rocket will perform a staging event and start burning the next stage.

Parameters

aDuration	The Specified duration to thrust.
aDeltaV	The calculated Delta-V.

Returns

The actual duration achieved.

References WsfRocketOrbitalManeuvering::GetTotalMass().

Referenced by ~Rocket().

---

The documentation for this class was generated from the following files:

• WsfRocketOrbitalManeuvering.hpp
• WsfRocketOrbitalManeuvering.cpp