Package org.orekit.propagation.events.functions

Class AbstractGeodeticEventFunction

java.lang.Object

org.orekit.propagation.events.functions.AbstractGeodeticEventFunction

All Implemented Interfaces:

EventFunction

Direct Known Subclasses:

AltitudeEventFunction, LatitudeValueCrossingFunction, LongitudeValueCrossingFunction

public abstract class AbstractGeodeticEventFunction
extends Object
implements EventFunction

Abstract class for event function related to geodetic coordinates.

Since:

14.0

Author:

Romain Serra

Constructor Summary

Constructors

Modifier	Constructor	Description
protected	AbstractGeodeticEventFunction(BodyShape body)	Constructor.

Method Summary

Modifier and Type	Method	Description
BodyShape	getBodyShape()	Getter for body shape.
protected <T extends CalculusFieldElement<T>> FieldGeodeticPoint<T>	transformToGeodeticPoint(FieldSpacecraftState<T> s)	Compute the geodetic coordinates (Field version).
protected GeodeticPoint	transformToGeodeticPoint(SpacecraftState s)	Compute the geodetic coordinates.

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

AbstractGeodeticEventFunction

protected AbstractGeodeticEventFunction(BodyShape body)

Constructor.

Parameters:

body - body

Method Details

getBodyShape

public BodyShape getBodyShape()

Getter for body shape.

Returns:

body

transformToGeodeticPoint

protected GeodeticPoint transformToGeodeticPoint(SpacecraftState s)

Compute the geodetic coordinates.

Parameters:

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

Returns:

geodetic point

transformToGeodeticPoint

protected <T extends CalculusFieldElement<T>>
FieldGeodeticPoint<T> transformToGeodeticPoint(FieldSpacecraftState<T> s)

Compute the geodetic coordinates (Field version).

Type Parameters:

T - field type

Parameters:

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

Returns:

geodetic point