Package org.orekit.attitudes

Class TabulatedLofOffset

java.lang.Object

org.orekit.attitudes.TabulatedLofOffset

All Implemented Interfaces:

AttitudeProvider, BoundedAttitudeProvider

public class TabulatedLofOffset
extends Object
implements BoundedAttitudeProvider

This class handles an attitude provider interpolating from a predefined table containing offsets from a Local Orbital Frame.

Instances of this class are guaranteed to be immutable.

Since:

7.1

Author:

Luc Maisonobe

See Also:

LofOffset, TabulatedProvider

Constructor Summary

Constructors

Constructor	Description
TabulatedLofOffset(Frame inertialFrame, LOF lof, List<? extends TimeStampedAngularCoordinates> table, int n, AngularDerivativesFilter filter)	Creates new instance.
TabulatedLofOffset(Frame inertialFrame, LOF lof, List<? extends TimeStampedAngularCoordinates> table, int n, AngularDerivativesFilter filter, AbsoluteDate minDate, AbsoluteDate maxDate)	Creates new instance.

Method Summary

Modifier and Type	Method	Description
<T extends CalculusFieldElement<T>> FieldAttitude<T>	getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
AbsoluteDate	getMaxDate()	Get the last date of the range.
AbsoluteDate	getMinDate()	Get the first date of the range.
List<? extends TimeStampedAngularCoordinates>	getTable()	Get an unmodifiable view of the tabulated attitudes.

Methods inherited from class java.lang.Object

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

Methods inherited from interface org.orekit.attitudes.AttitudeProvider

getAttitudeRotation, getAttitudeRotation

Constructor Detail

TabulatedLofOffset

public TabulatedLofOffset(Frame inertialFrame,
                          LOF lof,
                          List<? extends TimeStampedAngularCoordinates> table,
                          int n,
                          AngularDerivativesFilter filter)

Creates new instance.

This constructor uses the first and last point samples as the min and max dates.

Parameters:

inertialFrame - inertial frame with respect to which orbit should be computed

lof - local orbital frame

table - tabulated attitudes

n - number of attitude to use for interpolation

filter - filter for derivatives from the sample to use in interpolation

TabulatedLofOffset

public TabulatedLofOffset(Frame inertialFrame,
                          LOF lof,
                          List<? extends TimeStampedAngularCoordinates> table,
                          int n,
                          AngularDerivativesFilter filter,
                          AbsoluteDate minDate,
                          AbsoluteDate maxDate)

Creates new instance.

Parameters:

inertialFrame - inertial frame with respect to which orbit should be computed

lof - local orbital frame

table - tabulated attitudes

n - number of attitude to use for interpolation

minDate - min date to use

maxDate - max date to use

filter - filter for derivatives from the sample to use in interpolation

Since:

11.0

Method Detail

getTable

public List<? extends TimeStampedAngularCoordinates> getTable()

Get an unmodifiable view of the tabulated attitudes.

Returns:

unmodifiable view of the tabulated attitudes

getAttitude

public Attitude getAttitude(PVCoordinatesProvider pvProv,
                            AbsoluteDate date,
                            Frame frame)

Compute the attitude corresponding to an orbital state.

Specified by:

getAttitude in interface AttitudeProvider

Parameters:

pvProv - local position-velocity provider around current date

date - current date

frame - reference frame from which attitude is computed

Returns:

attitude on the specified date and position-velocity state

getAttitude

public <T extends CalculusFieldElement<T>> FieldAttitude<T> getAttitude(FieldPVCoordinatesProvider<T> pvProv,
                                                                        FieldAbsoluteDate<T> date,
                                                                        Frame frame)

Compute the attitude corresponding to an orbital state.

Specified by:

getAttitude in interface AttitudeProvider

Type Parameters:

T - type of the field elements

Parameters:

pvProv - local position-velocity provider around current date

date - current date

frame - reference frame from which attitude is computed

Returns:

attitude on the specified date and position-velocity state

getMinDate

public AbsoluteDate getMinDate()

Get the first date of the range.

Specified by:

getMinDate in interface BoundedAttitudeProvider

Returns:

the first date of the range

getMaxDate

public AbsoluteDate getMaxDate()

Get the last date of the range.

Specified by:

getMaxDate in interface BoundedAttitudeProvider

Returns:

the last date of the range