found::ApproximateOrbitPropagationAlgorithm Class Reference

OrbitPropagationAlgorithm is a stage that propagates an orbit over a specified time period. More...

#include <orbit.hpp>

Inheritance diagram for found::ApproximateOrbitPropagationAlgorithm:

Collaboration diagram for found::ApproximateOrbitPropagationAlgorithm:

Public Member Functions
	ApproximateOrbitPropagationAlgorithm (decimal totalTime, decimal dt, decimal radius, decimal mu)
	Constructs this OrbitPropagationAlgorithm.
	~ApproximateOrbitPropagationAlgorithm ()
	Destroys this.
LocationRecords	Run (const LocationRecords &data) override
	Projects an orbit.
Public Member Functions inherited from found::OrbitPropagationAlgorithm
	OrbitPropagationAlgorithm ()=default
	Constructs this.
virtual	~OrbitPropagationAlgorithm ()
	Destroys this.
Public Member Functions inherited from found::Stage< LocationRecords, LocationRecords >
	Stage ()=default
	Constructs a new Stage.
virtual	~Stage ()=default
	Destroys this.
void	DoAction () override
	Executes Run (with a stored input and storing the output)
LocationRecords &	GetResource ()
	Returns the stored input of this.
LocationRecords *&	GetProduct ()
	Returns the stored output of this.

Private Attributes
decimal	totalTime_
	The total time to predict over.
decimal	dt_
	The time step for integration (seconds)
decimal	radius_
	The radius of the celestial body (default is for Earth, in km)
decimal	mu_
	The gravitational parameter (default is for Earth in km^3/s^2)

Additional Inherited Members
Protected Attributes inherited from found::Stage< LocationRecords, LocationRecords >
LocationRecords	resource
	The stored input for this.
LocationRecords *	product
	The pointer to the stored output for this.

Detailed Description

OrbitPropagationAlgorithm is a stage that propagates an orbit over a specified time period.

It integrates the equations of motion to predict the satellite's trajectory using Runge-Kutta 4 (RK4).

Constructor & Destructor Documentation

ApproximateOrbitPropagationAlgorithm()

found::ApproximateOrbitPropagationAlgorithm::ApproximateOrbitPropagationAlgorithm ( decimal  totalTime, decimal  dt, decimal  radius, decimal  mu  )

inlineexplicit

Constructs this OrbitPropagationAlgorithm.

Parameters

totalTime	The total time to predict over
dt	The time step for integration (seconds)
radius	The radius of the celestial body (default is for Earth, in km)
mu	The gravitational parameter (default is for Earth in km^3/s^2)

~ApproximateOrbitPropagationAlgorithm()

found::ApproximateOrbitPropagationAlgorithm::~ApproximateOrbitPropagationAlgorithm

(

)

Destroys this.

Member Function Documentation

Run()

LocationRecords found::ApproximateOrbitPropagationAlgorithm::Run ( const LocationRecords &  data )

overridevirtual

Projects an orbit.

Parameters

data	The past data to use

Returns

Predicted positions in the future

Implements found::Stage< LocationRecords, LocationRecords >.

Member Data Documentation

dt_

decimal found::ApproximateOrbitPropagationAlgorithm::dt_

private

The time step for integration (seconds)

mu_

decimal found::ApproximateOrbitPropagationAlgorithm::mu_

private

The gravitational parameter (default is for Earth in km^3/s^2)

radius_

decimal found::ApproximateOrbitPropagationAlgorithm::radius_

private

The radius of the celestial body (default is for Earth, in km)

totalTime_

decimal found::ApproximateOrbitPropagationAlgorithm::totalTime_

private

The total time to predict over.

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

• src/orbit/orbit.hpp