org.orekit.propagation.semianalytical.dsst.forces

Class AbstractGaussianContributionContext

java.lang.Object

org.orekit.propagation.semianalytical.dsst.forces.ForceModelContext

org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

public class AbstractGaussianContributionContext
extends ForceModelContext

This class is a container for the common parameters used in AbstractGaussianContribution.

It performs parameters initialization at each integration step for the Gaussian contributions

Since:

10.0

Author:

Bryan Cazabonne

Field Summary

Fields

Modifier and Type	Field and Description
protected double	co2AB C / (2 * A * B) .
protected double	ooA 1 / A .
protected double	ooAB 1 / (A * B) .
protected double	ooBpo 1 / (1 + B) .
protected double	ooMu 1 / μ .
protected double	ton2a 2 / (n² * a) .

Method Summary

Modifier and Type	Method and Description
double	getCo2AB() Get co2AB = C / 2AB.
double	getMeanMotion() Get the Keplerian mean motion.
double	getMu() Get central attraction coefficient.
double	getOOA() Get ooA = 1 / A.
double	getOOAB() Get ooAB = 1 / (A * B).
double	getOoBpo() Get ooBpo = 1 / (B + 1).
double	getOoMU() Get ooMu = 1 / mu.
double	getTon2a() Get ton2a = 2 / (n² * a).

Methods inherited from class org.orekit.propagation.semianalytical.dsst.forces.ForceModelContext

getAuxiliaryElements

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Field Detail

ton2a

protected double ton2a

2 / (n² * a) .

ooA

protected double ooA

1 / A .

ooAB

protected double ooAB

1 / (A * B) .

co2AB

protected double co2AB

C / (2 * A * B) .

ooBpo

protected double ooBpo

1 / (1 + B) .

ooMu

protected double ooMu

1 / μ .

Method Detail

getMu

public double getMu()

Get central attraction coefficient.

Returns:

mu

getOOA

public double getOOA()

Get ooA = 1 / A.

Returns:

ooA

getOOAB

public double getOOAB()

Get ooAB = 1 / (A * B).

Returns:

ooAB

getCo2AB

public double getCo2AB()

Get co2AB = C / 2AB.

Returns:

co2AB

getOoBpo

public double getOoBpo()

Get ooBpo = 1 / (B + 1).

Returns:

ooBpo

getTon2a

public double getTon2a()

Get ton2a = 2 / (n² * a).

Returns:

ton2a

getOoMU

public double getOoMU()

Get ooMu = 1 / mu.

Returns:

ooMu

getMeanMotion

public double getMeanMotion()

Get the Keplerian mean motion.

The Keplerian mean motion is computed directly from semi major axis and central acceleration constant.

Returns:

Keplerian mean motion in radians per second