Package org.orekit.propagation.events.functions

Class AbstractGeodeticExtremumEventFunction

java.lang.Object

org.orekit.propagation.events.functions.AbstractGeodeticExtremumEventFunction

All Implemented Interfaces:

EventFunction

Direct Known Subclasses:

LatitudeExtremumEventFunction, LongitudeExtremumEventFunction

public abstract class AbstractGeodeticExtremumEventFunction
extends Object
implements EventFunction

Abstract class for geodetic coordinates extremum event function.

Since:

14.0

Author:

Romain Serra

Constructor Summary

Constructors

Modifier	Constructor	Description
protected	AbstractGeodeticExtremumEventFunction(BodyShape body)	Constructor.

Method Summary

Modifier and Type	Method	Description
BodyShape	getBodyShape()	Getter for body shape.
protected <T extends CalculusFieldElement<T>> FieldGeodeticPoint<FieldUnivariateDerivative1<T>>	transformToFieldGeodeticPoint(FieldSpacecraftState<T> s)	Compute the geodetic coordinates with automatic differentiation.
protected FieldGeodeticPoint<UnivariateDerivative1>	transformToFieldGeodeticPoint(SpacecraftState s)	Compute the geodetic coordinates with automatic differentiation.

Methods inherited from class java.lang.Object

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

Methods inherited from interface org.orekit.propagation.events.functions.EventFunction

dependsOnMainVariablesOnly, dependsOnTimeOnly, value, value

Constructor Details

AbstractGeodeticExtremumEventFunction

protected AbstractGeodeticExtremumEventFunction(BodyShape body)

Constructor.

Parameters:

body - body

Method Details

getBodyShape

public BodyShape getBodyShape()

Getter for body shape.

Returns:

body

transformToFieldGeodeticPoint

protected FieldGeodeticPoint<UnivariateDerivative1> transformToFieldGeodeticPoint(SpacecraftState s)

Compute the geodetic coordinates with automatic differentiation.

Parameters:

s - the current state information: date, kinematics, attitude

Returns:

geodetic point in Taylor Differential Algebra

transformToFieldGeodeticPoint

protected <T extends CalculusFieldElement<T>>
FieldGeodeticPoint<FieldUnivariateDerivative1<T>> transformToFieldGeodeticPoint(FieldSpacecraftState<T> s)

Compute the geodetic coordinates with automatic differentiation.

Type Parameters:

T - field type

Parameters:

s - the current state information: date, kinematics, attitude

Returns:

geodetic point in Taylor Differential Algebra