WsfConjunctionInput Class Reference

A class to setup a satellite so that it will suffer a conjunction at a given time with a given target. More...

#include <WsfConjunctionInput.hpp>

Public Member Functions
	WsfConjunctionInput ()
	WsfConjunctionInput (const WsfConjunctionInput &aOther)
WsfConjunctionInput &	operator= (const WsfConjunctionInput &aOther)=default
bool	ProcessInput (UtInput &aInput)
	Process the input file to setup the conjunction.
WsfConjunctionInput *	Clone () const
	Clone this object.
bool	SolutionFound () const
	Indicate if a solution to generate the conjunction was found.
const UtVec3d &	InitialLocationECI () const
	Return the initial location of the satellite.
const UtVec3d &	InitialVelocityECI () const
const UtVec3d &	SolutionVelocityECI () const
bool	Initialize (const UtCalendar &aTime, const ut::OrbitalState &aState)
void	ComputeSolution (const WsfSimulation &aSimulation, const UtCalendar &aTime, const UtOrbitalPropagatorBase &aInterceptorProp)

Detailed Description

A class to setup a satellite so that it will suffer a conjunction at a given time with a given target.

Constructor & Destructor Documentation

WsfConjunctionInput() [1/2]

WsfConjunctionInput::WsfConjunctionInput

(

)

Referenced by Clone(), operator=(), and WsfConjunctionInput().

WsfConjunctionInput() [2/2]

WsfConjunctionInput::WsfConjunctionInput

(

const WsfConjunctionInput &

aOther

)

References WsfConjunctionInput().

Member Function Documentation

Clone()

WsfConjunctionInput * WsfConjunctionInput::Clone

(

)

const

Clone this object.

References WsfConjunctionInput().

ComputeSolution()

void WsfConjunctionInput::ComputeSolution	(	const WsfSimulation &	aSimulation,
		const UtCalendar &	aTime,
		const UtOrbitalPropagatorBase &	aInterceptorProp )

Compute the solution for the initial velocity to provide the specified conjunction. This will solve the targeting problem to produce the input conjunction. This sets the solution velocity so that the spacecraft would move from the initial position to the position of the target spacecraft at the given time.

References WsfOrbitalTargeting::SetTolerance(), and WsfOrbitalTargeting::Solve().

Initialize()

bool WsfConjunctionInput::Initialize	(	const UtCalendar &	aTime,
		const ut::OrbitalState &	aState )

Initialize this object. This method will set the initial position and velocity for the solution. These kinematics will be used in the event that a conjunction solution is impossible. Unless the position and velocity are taken from other initialization, this will set the velocity to be the circular velocity for the specified position.

InitialLocationECI()

const UtVec3d & WsfConjunctionInput::InitialLocationECI ( ) const

inline

Return the initial location of the satellite.

InitialVelocityECI()

const UtVec3d & WsfConjunctionInput::InitialVelocityECI ( ) const

inline

Return the initial velocity of the satellite. This velocity is what the satellite will have if the conjunction solution is impossible for some reason (e.g. the orbit hits the Earth).

operator=()

WsfConjunctionInput & WsfConjunctionInput::operator= ( const WsfConjunctionInput & aOther )

default

References WsfConjunctionInput().

ProcessInput()

bool WsfConjunctionInput::ProcessInput

(

UtInput &

aInput

)

Process the input file to setup the conjunction.

SolutionFound()

bool WsfConjunctionInput::SolutionFound ( ) const

inline

Indicate if a solution to generate the conjunction was found.

SolutionVelocityECI()

const UtVec3d & WsfConjunctionInput::SolutionVelocityECI ( ) const

inline

return the solution velocity of the satellite. This velocity if what the satellite will have if the conjunction solution is successful.

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

• WsfConjunctionInput.hpp
• WsfConjunctionInput.cpp