Class FieldDSSTTesseralContext<T extends CalculusFieldElement<T>>
- java.lang.Object
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- org.orekit.propagation.semianalytical.dsst.forces.FieldForceModelContext<T>
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- org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext<T>
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- org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext<T>
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- Type Parameters:
T
- type of the field elements
public class FieldDSSTTesseralContext<T extends CalculusFieldElement<T>> extends FieldDSSTGravityContext<T>
This class is a container for the common "field" parameters used inDSSTTesseral
.It performs parameters initialization at each integration step for the Tesseral contribution to the central body gravitational perturbation.
- Since:
- 10.0
- Author:
- Bryan Cazabonne
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Method Summary
All Methods Instance Methods Concrete Methods Deprecated Methods Modifier and Type Method Description T
getE2()
Get ecc².T
getMoa()
Deprecated.since 12.2 Use getMuoa() insteadT
getOrbitPeriod()
Get the Keplerian period.T
getRatio()
Get the ratio of satellite period to central body rotation period.T
getTheta()
Get Central body rotation angle θ.-
Methods inherited from class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
getA, getAlpha, getAx2oA, getBeta, getBoA, getBoABpo, getBodyFixedToInertialTransform, getChi, getChi2, getCo2AB, getGamma, getMeanMotion, getMuoa, getOoAB, getRoa
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Methods inherited from class org.orekit.propagation.semianalytical.dsst.forces.FieldForceModelContext
getFieldAuxiliaryElements
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Method Detail
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getE2
public T getE2()
Get ecc².- Returns:
- e2
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getTheta
public T getTheta()
Get Central body rotation angle θ.- Returns:
- theta
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getMoa
@Deprecated public T getMoa()
Deprecated.since 12.2 Use getMuoa() insteadGet μ / a .- Returns:
- moa
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getOrbitPeriod
public T getOrbitPeriod()
Get the Keplerian period.The Keplerian period is computed directly from semi major axis and central acceleration constant.
- Returns:
- Keplerian period in seconds, or positive infinity for hyperbolic orbits
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getRatio
public T getRatio()
Get the ratio of satellite period to central body rotation period.- Returns:
- ratio
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