Package org.orekit.files.general

Interface AttitudeEphemerisFile.AttitudeEphemerisSegment<C extends TimeStampedAngularCoordinates>

Type Parameters:

C - type of the angular coordinates

All Known Implementing Classes:

AemSegment, AttitudeStateHistory, OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment

Enclosing interface:

AttitudeEphemerisFile<C extends TimeStampedAngularCoordinates,S extends AttitudeEphemerisFile.AttitudeEphemerisSegment<C>>

public static interface AttitudeEphemerisFile.AttitudeEphemerisSegment<C extends TimeStampedAngularCoordinates>

A segment of an attitude ephemeris for a satellite.

Segments are typically used to split an ephemeris around discontinuous events such as maneuvers.

Since:

10.3

Author:

Raphaël Fermé

See Also:

AttitudeEphemerisFile, AttitudeEphemerisFile.SatelliteAttitudeEphemeris

Method Summary

Modifier and Type	Method	Description
List<C>	getAngularCoordinates()	Get an unmodifiable list of attitude data lines.
BoundedAttitudeProvider	getAttitudeProvider()	Get the attitude provider for this attitude ephemeris segment.
AngularDerivativesFilter	getAvailableDerivatives()	Get which derivatives of angular data are available in this attitude ephemeris segment.
String	getInterpolationMethod()	Get the interpolation method to be used.
int	getInterpolationSamples()	Get the number of samples to use in interpolation.
Frame	getReferenceFrame()	Get the reference frame from which attitude is defined.
AbsoluteDate	getStart()	Get the start date of this ephemeris segment.
AbsoluteDate	getStop()	Get the end date of this ephemeris segment.

Method Detail

getAngularCoordinates

List<C> getAngularCoordinates()

Get an unmodifiable list of attitude data lines.

Returns:

a list of attitude data

getReferenceFrame

Frame getReferenceFrame()

Get the reference frame from which attitude is defined.

Returns:

the reference frame from which attitude is defined

getStart

AbsoluteDate getStart()

Get the start date of this ephemeris segment.

Returns:

ephemeris segment start date.

getStop

AbsoluteDate getStop()

Get the end date of this ephemeris segment.

Returns:

ephemeris segment end date.

getInterpolationMethod

String getInterpolationMethod()

Get the interpolation method to be used.

Returns:

the interpolation method

getInterpolationSamples

int getInterpolationSamples()

Get the number of samples to use in interpolation.

Returns:

the number of points to use for interpolation.

getAvailableDerivatives

AngularDerivativesFilter getAvailableDerivatives()

Get which derivatives of angular data are available in this attitude ephemeris segment.

Returns:

a value indicating if the file contains rotation and/or rotation rate and/or acceleration data.

getAttitudeProvider

BoundedAttitudeProvider getAttitudeProvider()

Get the attitude provider for this attitude ephemeris segment.

Returns:

the attitude provider for this attitude ephemeris segment.