org.orekit.orbits

Class AbstractOrbitInterpolator

java.lang.Object

org.orekit.time.AbstractTimeInterpolator<Orbit>

org.orekit.orbits.AbstractOrbitInterpolator

All Implemented Interfaces:

TimeInterpolator<Orbit>

Direct Known Subclasses:

OrbitBlender, OrbitHermiteInterpolator

public abstract class AbstractOrbitInterpolator
extends AbstractTimeInterpolator<Orbit>

Abstract class for orbit interpolator.

Author:

Vincent Cucchietti

Nested Class Summary

Nested classes/interfaces inherited from class org.orekit.time.AbstractTimeInterpolator

AbstractTimeInterpolator.InterpolationData

Field Summary

Fields inherited from class org.orekit.time.AbstractTimeInterpolator

DEFAULT_EXTRAPOLATION_THRESHOLD_SEC, DEFAULT_INTERPOLATION_POINTS

Constructor Summary

Constructors

Constructor and Description
AbstractOrbitInterpolator(int interpolationPoints, double extrapolationThreshold, Frame outputInertialFrame) Constructor.

Method Summary

Modifier and Type	Method and Description
static void	checkOrbitsConsistency(Collection<Orbit> sample) Check orbits consistency by comparing their gravitational parameters µ.
Frame	getOutputInertialFrame() Get output inertial frame.
Orbit	interpolate(AbsoluteDate interpolationDate, Collection<Orbit> sample) Get an interpolated instance.

Methods inherited from class org.orekit.time.AbstractTimeInterpolator

addOptionalSubInterpolatorIfDefined, checkInterpolatorCompatibilityWithSampleSize, getExtrapolationThreshold, getNbInterpolationPoints, getSubInterpolators, getTimeParameter, interpolate, interpolate

Methods inherited from class java.lang.Object

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

Constructor Detail

AbstractOrbitInterpolator

public AbstractOrbitInterpolator(int interpolationPoints,
                                 double extrapolationThreshold,
                                 Frame outputInertialFrame)

Constructor.

Parameters:

interpolationPoints - number of interpolation points

extrapolationThreshold - extrapolation threshold beyond which the propagation will fail

outputInertialFrame - output inertial frame

Method Detail

checkOrbitsConsistency

public static void checkOrbitsConsistency(Collection<Orbit> sample)

Check orbits consistency by comparing their gravitational parameters µ.

Parameters:

sample - orbits sample

interpolate

public Orbit interpolate(AbsoluteDate interpolationDate,
                         Collection<Orbit> sample)

Get an interpolated instance...

Specified by:

interpolate in interface TimeInterpolator<Orbit>

Overrides:

interpolate in class AbstractTimeInterpolator<Orbit>

Parameters:

interpolationDate - interpolation date

sample - time stamped sample

Returns:

a new instance, interpolated at specified date

getOutputInertialFrame

public Frame getOutputInertialFrame()

Get output inertial frame.

Returns:

output inertial frame