AbstractGeodeticExtremumEventFunction (OREKIT 14.0-SNAPSHOT API)

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

All Methods Instance Methods Concrete Methods
Modifier and Type	Method	Description
`BodyShape`	`getBodyShape()`	Getter for body shape.
`protected <T extends CalculusFieldElement<T>> FieldGeodeticPoint<FieldUnivariateDerivative2<T>>`	`transformToFieldGeodeticPoint(FieldSpacecraftState<T> s)`	Compute the geodetic coordinates with automatic differentiation.
`protected FieldGeodeticPoint<UnivariateDerivative2>`	`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 Detail
  - AbstractGeodeticExtremumEventFunction
```
protected AbstractGeodeticExtremumEventFunction(BodyShape body)
```
    Constructor.
    
    Parameters:
    
    body - body
- Method Detail
  - getBodyShape
```
public BodyShape getBodyShape()
```
    Getter for body shape.
    
    Returns:
    
    body
  - transformToFieldGeodeticPoint
```
protected FieldGeodeticPoint<UnivariateDerivative2> 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<FieldUnivariateDerivative2<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