User Manual 3.3 Attitude leg : Différence entre versions

De Wiki
Aller à : navigation, rechercher
(Package Overview)
(Scope)
Ligne 5 : Ligne 5 :
 
The purpose of this chapter is to describe the current Patrius attitude legs.
 
The purpose of this chapter is to describe the current Patrius attitude legs.
  
An attitude leg is a time-bounded attitude law. Generalities on attitude laws can be found [ATT_ALW_Home here].
+
An attitude leg is a time-bounded attitude law. Generalities on attitude laws can be found [User Manual 3.3 Attitude law|here].
  
 
=== Javadoc ===
 
=== Javadoc ===

Version du 28 février 2018 à 15:09


Introduction

Scope

The purpose of this chapter is to describe the current Patrius attitude legs.

An attitude leg is a time-bounded attitude law. Generalities on attitude laws can be found [User Manual 3.3 Attitude law|here].

Javadoc

Library Javadoc
Orekit Package org.orekit.attitudes
Orekit addons Package org.orekit.attitudes

Links

Orekit Attitudes architecture description, Orekit site.

Useful Documents

Modèle:SpecialInclusion prefix=$theme sub section="UsefulDocs"/

Package Overview

The attitude leg AttitudeLeg interface inherits the AttitudeProvider interface. Its place in the global Attitude design can be found here.

Features Description

Generalities

Attitude legs inherit the interface AttitudeLeg. They are time-bounded attitude providers. In addition to AttitudeProvider services, they provide the method getTimeInterval() returning the leg timespan.

Available attitude leg

Attitude legs sequence

An attitude legs sequence is a container for several attitude legs, contiguous for their time intervals, in such a way that the attitude legs sequence can be processed like a single attitude leg by the propagator.

The attitude legs sequence is the equivalent of the [ATT_ALW_Home#HAttitudessequence Attitudes sequence], using attitude legs (AttitudeLeg instances) rather than attitude laws (AttitudeLaw instances). The switching from one attitude leg to another is based on the time interval of validity of the two legs.

An attitude legs sequence is associated to a PVCoordinatesProvider instance, which will override any PVCoordinatesProvider passed as parameter to the methods like getAttitude(). The reason for such a behaviour, which violates the contract of the AttitudeProvider interface, is that :

  • an attitude legs sequence needs to enforce coherence between its inner attitude legs and its homing maneuvers.
  • homing maneuvers are created and computed once by using a specific PVCoordinatesProvider, in order to preserve good performances.

Therefore, the attitude legs sequence can only compute attitudes with the PVCoordinatesProvider instance it was built with, and the inner attitude legs should be coherent with this provider (the attitude sequence does not check if it's the case!)

TabulatedAttitude

TabulatedAttitude is an implementation of AttitudeLeg. It represents a tabulated attitude leg.

In order to interpolate the attitude at a date, the user must specify a list of ordered attitudes, and can specify a number of points used by Hermite interpolation. If not specified, the number of points used by Hermite interpolation is set to a default number (currently 2).

final List<Attitude> attList = new ArrayList<Attitude>();
attList.add(attitude0);
attList.add(attitude1);
final int nbrInterpPoints = 2;
final TabulatedAttitude attLeg = new TabulatedAttitude(attList, nbrInterpPoints);

It is possible to get the non-interpolated ordered attitudes :

final List<Attitude> attitudes = attLeg.getAttitudes();

Once the tabulated is defined, the computation can be performed on any orbital state using getAttitude() method:

Attitude attitude = attLeg.getAttitude(orbit, date, FramesFactory.getEME2000());

RelativeTabulatedAttitudeLeg

RelativeTabulatedAttitudeLeg is an implementation of AttitudeLeg. An instance of RelativeTabulatedAttitudeLeg can be created with a List<Pair<Double, Rotation>> or with a List<Pair<Double, AngularCoordinates>>. Each Rotation (or AngularCoordinates) is associated with a double representing its time ellapsed in seconds since the reference date. Here is an example of a creation of an instance of RelativeTabulatedAttitudeLeg :

// date and frame
AbsoluteDate refDate = new AbsoluteDate(2008, 1, 1, TimeScalesFactory.getTAI());
Frame frame = FramesFactory.getGCRF();
double timeEllapsedSinceRefDate = 1.0;
 
// List of AR
List<Pair<Double, AngularCoordinates>> listAr = new ArrayList<Pair<Double, AngularCoordinates>>();
final AngularCoordinates ar = new AngularCoordinates(
                new Rotation(false, 0.48, 0.64, 0.36, 0.48), Vector3D.PLUS_I, Vector3D.PLUS_J);
listAr.add(new Pair<Double, AngularCoordinates>(timeEllapsedSinceRefDate, ar));
 
// create RelativeTabulatedAttitudeLeg
final RelativeTabulatedAttitudeLeg relativeTabulatedAttitudeLeg = 
                new RelativeTabulatedAttitudeLeg(refDate, frame, listAr);

Getting Started

Building an attitude legs sequence

The attitude legs sequence was designed as a simple container, it performs only a few coherence checks on its inner attitude laws. Here's how an attitude sequence is built.

  • An attitude legs sequence is created empty, associated to a single PVCoordinatesProvider instance.
  • The sequence is mutable, attitude laws can be added to it one by one.
  • Each attitude law is identified by a code.
  • The sequence has a validity time interval, which is the grouping of the validity time intervals of all contained laws.
  • The time interval of a newly added law must be contiguous to the grouped time interval of the already added laws. Otherwise an OrekitException is thrown.
  • As soon as the sequence contains at least one law, methods of the AttitudeLeg interface can be called on the attitude sequence. The attitude sequence forwards the request to the appropriate attitude leg (according to the asking date), but replaces the PVCoordinatesProvider attribute of the call with the inner PVCoordinatesProvider instance.

AttitudeLawLeg and AttitudeLegsSequence : Code sample

final BodyCenterPointing earthCenterAttitudeLaw = new BodyCenterPointing(itrf);
final AttitudeLeg law1 = new AttitudeLawLeg(earthCenterAttitudeLaw, date1, date2);
final AttitudeLeg law2 = ... ;
final AttitudeLeg law3 = ... ;
 
PVCoordinatesProvider pvProvider = new CartesianOrbit(pvCoordinates, gcrf, date1, mu);
final AttitudeLegsSequence sequence = new AttitudeLegsSequence(pvProvider);
// After each add the sequence has to be contiguous, so the order may be important
sequence.add("L1", law1);
sequence.add("L2", law2);
sequence.add("L3", law3);
 
// Call to getAttitude on the sequence ignores otherPvProvider and uses pvProvider internally instead
final Attitude sAttitude = sequence.getAttitude(otherPvProvider, date, itrf);

Contents

Interfaces

Interface Summary Javadoc
AttitudeLeg This interface extends the AttitudeProvider interface and adds the time interval of validity notion to the attitude laws. ...

Classes

Class Summary Javadoc
AttitudeLawLeg Object representing an attitude law for spacecraft attitude field purposes. ...
TabulatedAttitude Object representing a tabulated attitude leg : the attitude at a date is interpolated from a list of known ones. ...
AttitudeLegsSequence Object representing a sequence of contiguous attitude legs. ...
RelativeTabulatedAttitudeLeg This class implements a tabulated attitude leg with relative dates. ...