User Manual 4.0 Multi Propagation - Historique des versions

Admin le 21 février 2018 à 14:24

2018-02-21T14:24:15Z

Admin : /* Contents */

2018-02-21T10:44:52Z

Contents

← Version précédente		Version du 21 février 2018 à 10:44
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	== Contents ==		== Contents ==
	=== Interfaces ===		=== Interfaces ===
	\|=~~(% colspan~~="3" %)Interface~~\|=(% colspan~~="6" %)Summary~~\|=(% colspan~~="1" %)Javadoc		{\| class="wikitable"
	\|~~(% colspan="3" %)~~**MultiPropagator\|~~(% colspan="6" %)~~This interface provides a way to propagate several states at any time.\|~~(% colspan="1" %)~~[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/MultiPropagator.html ...]		\|-
	\|~~(% colspan="3" %)~~**MultiModeHandler\|~~(% colspan="6" %)~~Common interface for all multi propagator mode handlers initialization.\|~~(% colspan="1" %)~~[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/numerical/multi/MultiModeHandler.html ...]		! scope="col"\| Interface
			! scope="col"\| Summary
			! scope="col"\| Javadoc
			\|-
			\|**MultiPropagator
			\|This interface provides a way to propagate several states at any time.
			\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/MultiPropagator.html ...]
			\|-
			\|**MultiModeHandler
			\|Common interface for all multi propagator mode handlers initialization.
			\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/numerical/multi/MultiModeHandler.html ...]
			\|}

	=== Classes ===		=== Classes ===
	\|=~~(% colspan~~="3" %)Class~~\|=(% colspan~~="6" %)Summary~~\|=(% colspan~~="1" %)Javadoc		{\| class="wikitable"
	\|~~(% colspan="3" %)~~'''SpacecraftState'''\|~~(% colspan="6" %)~~This class is the representation of a complete state holding orbit, attitude for forces and for events computation and additional states at a given date.\|~~(% colspan="1" %)~~{{~~JDLink label="~~.~~.." jd="OR" suffix="~~fr/cnes/sirius/patrius/propagation		\|-
	/SpacecraftState.html~~"/}}~~		! scope="col"\| Class
	\|~~(% colspan="3" %)~~'''MultiNumericalPropagator'''\|~~(% colspan="6" %)~~This class propagates several SpacecraftState using numerical integration.\|~~(% colspan="1" %)~~[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/numerical/multi/MultiNumericalPropagator.html ...]		! scope="col"\| Summary
	\|~~(% colspan="3" %)~~'''AttitudeEquation'''\|~~(% colspan="6" %)~~This class represents attitude differential equations.\|~~(% colspan="1" %)~~{{~~JDLink label="~~.~~.." jd="OR" suffix="~~fr/cnes/sirius/patrius/propagation		! scope="col"\| Javadoc
	/numerical/AttitudeEquation.html~~"/}}~~		\|-
	\|~~(% colspan="3" %)~~'''MultiIntegratedEphemeris'''\|~~(% colspan="6" %)~~This class stores sequentially generated orbital parameters for later retrieval.\|~~(% colspan="1" %)~~[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/precomputed/multi/MultiIntegratedEphemeris.html ...]		\|'''SpacecraftState'''
			\|This class is the representation of a complete state holding orbit, attitude for forces and for events computation and additional states at a given date.
			\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/SpacecraftState.html ...]
			\|-
			\|'''MultiNumericalPropagator'''
			\|This class propagates several SpacecraftState using numerical integration.
			\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/numerical/multi/MultiNumericalPropagator.html ...]
			\|-
			\|'''AttitudeEquation'''
			\|This class represents attitude differential equations.
			\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/numerical/AttitudeEquation.html ...]
			\|-
			\|'''MultiIntegratedEphemeris'''
			\|This class stores sequentially generated orbital parameters for later retrieval.
			\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/precomputed/multi/MultiIntegratedEphemeris.html ...]
			\|}

	[[Category:User_Manual_4.0_Orbit_Propagation]]		[[Category:User_Manual_4.0_Orbit_Propagation]]

Admin : /* Javadoc */

2018-02-21T10:40:39Z

Javadoc

← Version précédente		Version du 21 février 2018 à 10:40
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	All the classes related to numerical propagation are in the <code>fr.cnes.sirius.patrius.propagation.numerical.multi</code> package of the Patrius library. The classes related to events detection are in the package <code>fr.cnes.sirius.patrius.propagation.events.multi</code> of the Patrius library. But the interface for multi event detectors is in <code>fr.cnes.sirius.patrius.propagation.events.multi</code> package of the Patrius library.		All the classes related to numerical propagation are in the <code>fr.cnes.sirius.patrius.propagation.numerical.multi</code> package of the Patrius library. The classes related to events detection are in the package <code>fr.cnes.sirius.patrius.propagation.events.multi</code> of the Patrius library. But the interface for multi event detectors is in <code>fr.cnes.sirius.patrius.propagation.events.multi</code> package of the Patrius library.

	\|=~~(% colspan~~="3" %)Library~~\|=(% colspan~~="6" %)Javadoc
	\|~~(% colspan="3" %)~~Patrius \|~~(% colspan="6" %)~~[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/events/multi/package-summary.html Package fr.cnes.sirius.patrius.propagation.events.multi]		{\| class="wikitable"
	\|~~(% colspan="3" %)~~Patrius\|~~(% colspan="6" %)~~[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/events/multi/package-summary.html Package fr.cnes.sirius.patrius.events.multi]		\|-
	\|~~(% colspan="3" %)~~Patrius\|~~(% colspan="6" %)~~[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/events/multi/package-summary.html Package fr.cnes.sirius.patrius.propagation.events.multi]		! scope="col"\| Library
	\|~~(% colspan="3" %)~~Patrius\|~~(% colspan="6" %)~~[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/numerical/multi/package-summary.html Package fr.cnes.sirius.patrius.propagation.numerical.multi]		! scope="col"\| Javadoc
	\|~~(% colspan="3" %)~~Patrius\|~~(% colspan="6" %)~~[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/precomputed/multi/package-summary.html Package fr.cnes.sirius.patrius.propagation.precomputed.multi]		\|-
	\|~~(% colspan="3" %)~~Patrius\|~~(% colspan="6" %)~~[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/sampling/multi/package-summary.html Package fr.cnes.sirius.patrius.propagation.sampling.multi]		\|Patrius
			\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/events/multi/package-summary.html Package fr.cnes.sirius.patrius.propagation.events.multi]
			\|-
			\|Patrius
			\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/events/multi/package-summary.html Package fr.cnes.sirius.patrius.events.multi]
			\|-
			\|Patrius
			\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/events/multi/package-summary.html Package fr.cnes.sirius.patrius.propagation.events.multi]
			\|-
			\|Patrius
			\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/numerical/multi/package-summary.html Package fr.cnes.sirius.patrius.propagation.numerical.multi]
			\|-
			\|Patrius
			\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/precomputed/multi/package-summary.html Package fr.cnes.sirius.patrius.propagation.precomputed.multi]
			\|-
			\|Patrius
			\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/sampling/multi/package-summary.html Package fr.cnes.sirius.patrius.propagation.sampling.multi]
			\|}

	=== Links ===		=== Links ===

Admin le 19 février 2018 à 16:36

2018-02-19T16:36:41Z

← Version précédente		Version du 19 février 2018 à 16:36
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	== Introduction ==		== Introduction ==
	=== Scope ===		=== Scope ===
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	/numerical/AttitudeEquation.html"/}}		/numerical/AttitudeEquation.html"/}}
	\|(% colspan="3" %)'''MultiIntegratedEphemeris'''\|(% colspan="6" %)This class stores sequentially generated orbital parameters for later retrieval.\|(% colspan="1" %)[{{PathCurrentJavaDoc}}/fr/cnes/sirius/patrius/propagation/precomputed/multi/MultiIntegratedEphemeris.html ...]		\|(% colspan="3" %)'''MultiIntegratedEphemeris'''\|(% colspan="6" %)This class stores sequentially generated orbital parameters for later retrieval.\|(% colspan="1" %)[{{PathCurrentJavaDoc}}/fr/cnes/sirius/patrius/propagation/precomputed/multi/MultiIntegratedEphemeris.html ...]

			[[Category:User_Manual_4.0_Orbit_Propagation]]

Admin : /* Add event detector */

2018-02-19T16:35:44Z

Add event detector

← Version précédente		Version du 19 février 2018 à 16:35
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	=== Add event detector ===		=== Add event detector ===
	The user could add :		The user could add :
	*an [{{PathCurrentJavaDoc}}/fr/cnes/sirius/patrius/propagation/events/EventDetector.html EventDetector] associated with a specific state using'''''addEventDetector(EventDetector, String)'''''		*an [{{PathCurrentJavaDoc}}/fr/cnes/sirius/patrius/propagation/events/EventDetector.html EventDetector] associated with a specific state using '''''addEventDetector(EventDetector, String)'''''
	*a [{{PathCurrentJavaDoc}}/fr/cnes/sirius/patrius/propagation/events/multi/MultiEventDetector.html MultiEventDetector] associated with several states added to the propagator using'''''addEventDetector(MultiEventDetector)'''''		*a [{{PathCurrentJavaDoc}}/fr/cnes/sirius/patrius/propagation/events/multi/MultiEventDetector.html MultiEventDetector] associated with several states added to the propagator using '''''addEventDetector(MultiEventDetector)'''''

	See [MIS_EVT_Home events presentation ] and [MIS_MEVEN_Home multi events presentation ] chapters for more details.		See [MIS_EVT_Home events presentation] and [MIS_MEVEN_Home multi events presentation] chapters for more details.

	== Contents ==		== Contents ==

Admin : /* Set the central attraction coefficient */

2018-02-19T16:34:59Z

Set the central attraction coefficient

← Version précédente		Version du 19 février 2018 à 16:34
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	=== Set the central attraction coefficient ===		=== Set the central attraction coefficient ===
	For each state, the central attraction coefficient used in the integration process could be defined with the method'''''setMu(double, String)'''''.		For each state, the central attraction coefficient used in the integration process could be defined with the method '''''setMu(double, String)'''''.
	If for a specific state, this method was not called, the central attraction coefficient of the orbit is used in the integration process.		If for a specific state, this method was not called, the central attraction coefficient of the orbit is used in the integration process.<br>
	T and '''''getFrame(String)'''''.		The central attraction coefficient and the frame used in the integration process could be retrieved for a specific state using '''''getMu(String)''''' and '''''getFrame(String)'''''.

	<syntaxhighlight lang="java">		<syntaxhighlight lang="java">

Admin : /* Propagate the attitude */

2018-02-19T16:33:44Z

Propagate the attitude

← Version précédente		Version du 19 février 2018 à 16:33
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	=== Propagate the attitude ===		=== Propagate the attitude ===

	As for the [{{PathCurrentJavaDoc}}/fr/cnes/sirius/patrius/propagation/numerical/NumericalPropagator.html NumericalPropagator], to propagate the [{{PathCurrentJavaDoc}}//fr/cnes/sirius/patrius/attitudes/Attitude.html Attitude] of a specific state, two treatments could be applied :		As for the [{{PathCurrentJavaDoc}}/fr/cnes/sirius/patrius/propagation/numerical/NumericalPropagator.html NumericalPropagator], to propagate the [{{PathCurrentJavaDoc}}/fr/cnes/sirius/patrius/attitudes/Attitude.html Attitude] of a specific state, two treatments could be applied :
	*compute the attitude with an [{{PathCurrentJavaDoc}}''fr/cnes/sirius/patrius/attitudes/AttitudeProvider.html AttitudeProvider] :'''''setAttitudeProvider(AttitudeProvider, String)//'''.
	It is possible to deals with :		*compute the attitude with an [{{PathCurrentJavaDoc}}/fr/cnes/sirius/patrius/attitudes/AttitudeProvider.html AttitudeProvider] : '''''setAttitudeProvider(AttitudeProvider, String)'''''.<br>It is possible to deals with :
	**a single attitude by calling'''''setAttitudeProvider(AttitudeProvider, String)'''''		**a single attitude by calling '''''setAttitudeProvider(AttitudeProvider, String)'''''
	~~'''~~two attitudes by calling'''''setAttitudeProviderForces(AttitudeProvider, String)''''' or '''''setAttitudeProviderEvents(AttitudeProvider, String)''. It is not possible to call ''setAttitudeProvider(AttitudeProvider, String)'' and ''setAttitudeProviderForces(AttitudeProvider, String)'' (or ''setAttitudeProviderEvents(AttitudeProvider, String)''**)		**two attitudes by calling '''''setAttitudeProviderForces(AttitudeProvider, String)''''' or '''''setAttitudeProviderEvents(AttitudeProvider, String)'''''. It is not possible to call '''''setAttitudeProvider(AttitudeProvider, String)''''' and '''''setAttitudeProviderForces(AttitudeProvider, String)''''' (or '''''setAttitudeProviderEvents(AttitudeProvider, String)''''')
	*propagate the attitude as a 7-dimension additional state :'''''addAttitudeEquation(AttitudeEquation, String)'''''.		*propagate the attitude as a 7-dimension additional state : '''''addAttitudeEquation(AttitudeEquation, String)'''''.<br>In practical terms, the user has to build the additional equation by extending the abstract class [{{PathCurrentJavaDoc}}/fr/cnes/sirius/patrius/propagation/numerical/AttitudeEquation.html AttitudeEquation], call '''''addAttitudeEquation(AttitudeEquation, String)'''''.
	In practical terms, the user has to build the additional equation by extending the abstract class [{{PathCurrentJavaDoc}}''fr/cnes/sirius/patrius/propagation/numerical/AttitudeEquation.html AttitudeEquation], call'''''addAttitudeEquation(AttitudeEquation, String)//'''.

	See [ORB_PRO_UseP mono numerical propagation] chapter for more details.		See [ORB_PRO_UseP mono numerical propagation] chapter for more details.

Admin : /* Add additional equations */

2018-02-19T16:30:09Z

Add additional equations

← Version précédente		Version du 19 février 2018 à 16:30
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	=== Add additional equations ===		=== Add additional equations ===
	As for the {{~~JDLink label="NumericalPropagator" jd="PS" suffix="~~fr/cnes/sirius/patrius/propagation		As for the [{{PathCurrentJavaDoc}}/fr/cnes/sirius/patrius/propagation/numerical/NumericalPropagator.html NumericalPropagator], additional equations corresponding to the additional states of each states should be added to the propagator.
	/numerical/NumericalPropagator.html~~"/}}~~, additional equations corresponding to the additional states of each states should be added to the propagator.

	These additional equations are given to the multi numerical propagator for a specific state thanks to the following methods :		These additional equations are given to the multi numerical propagator for a specific state thanks to the following methods :

Admin : /* Add additional equations */

2018-02-19T16:28:51Z

Add additional equations

← Version précédente		Version du 19 février 2018 à 16:28
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	These additional equations are given to the multi numerical propagator for a specific state thanks to the following methods :		These additional equations are given to the multi numerical propagator for a specific state thanks to the following methods :

	*''addAdditionalEquation(AdditionalEquation, String)''		*'''''addAdditionalEquation(AdditionalEquation, String)'''''
	'''*''addAttitudeEquation(AttitudeEquation, String)'''''		*'''''addAttitudeEquation(AttitudeEquation, String)'''''
	*''setMassProviderEquation(MassProvider, String)'' (This method should be called only once, mass provider must be mass provider used in force models)		*'''''setMassProviderEquation(MassProvider, String)''''' (This method should be called only once, mass provider must be mass provider used in force models)

	The method'''''setAdditionalStateTolerance(String, double[], double[])''''' may be used to add variation tolerance values (absolute and relative) to a specific additional state.		The method '''''setAdditionalStateTolerance(String, double[], double[])''''' may be used to add variation tolerance values (absolute and relative) to a specific additional state.

	For each state, the additional states should correspond with the added additional equations (same name, same size).		For each state, the additional states should correspond with the added additional equations (same name, same size).

Admin : /* Add initial states */

2018-02-19T16:27:33Z

Add initial states

← Version précédente		Version du 19 février 2018 à 16:27
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	=== Add initial states ===		=== Add initial states ===
	Initial states could be added to the propagator using the method'''''addInitialState(SpacecraftState, String)'''''. Each added state is defined by a unique ID. An error is raised if :		Initial states could be added to the propagator using the method '''''addInitialState(SpacecraftState, String)'''''. Each added state is defined by a unique ID. An error is raised if :
	* the input spacecraft ID is empty or null.		* the input spacecraft ID is empty or null.
	* a state with the same ID was already added to the propagator.		* a state with the same ID was already added to the propagator.
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	Note that, the initial state should be added before adding an additional equation, an attitude provider, a force model, an event ... etc ... associated with this state. Otherwise, the input spacecraft Id will not be recognized.		Note that, the initial state should be added before adding an additional equation, an attitude provider, a force model, an event ... etc ... associated with this state. Otherwise, the input spacecraft Id will not be recognized.

	The map of the added states could be retrieved with'''''getInitialStates()'''''		The map of the added states could be retrieved with '''''getInitialStates()'''''

	=== Add additional equations ===		=== Add additional equations ===

← Version précédente		Version du 21 février 2018 à 14:24
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	==== Multi Numerical Propagator ====		==== Multi Numerical Propagator ====

	The multi propagator architecture is copied from [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/Propagator.html Propagator] interface and [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/numerical/NumericalPropagator.html NumericalPropagator] class, and added to PATRIUS library.		The multi propagator architecture is copied from [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/Propagator.html Propagator] interface and [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/numerical/NumericalPropagator.html NumericalPropagator] class, and added to PATRIUS library.

	[[File:MultiNumericalPropagator.png\|center\|600px]]		[[File:MultiNumericalPropagator.png\|center\|600px]]
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	== Features Description ==		== Features Description ==
	The PATRIUS library offers a [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/numerical/multi/MultiNumericalPropagator.html multi numerical propagator]. It aims at propagating several [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/SpacecraftState.html SpacecraftState] at the same time using numerical propagation. The N [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/SpacecraftState.html SpacecraftState] are propagated during the same time interval using the same [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/math/ode/FirstOrderIntegrator.html FirstOrderIntegrator].		The PATRIUS library offers a [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/numerical/multi/MultiNumericalPropagator.html multi numerical propagator]. It aims at propagating several [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/SpacecraftState.html SpacecraftState] at the same time using numerical propagation. The N [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/SpacecraftState.html SpacecraftState] are propagated during the same time interval using the same [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/math/ode/FirstOrderIntegrator.html FirstOrderIntegrator].

	Each state is identified with an ID of type String. All states can be completely different but they should have the same internal date.		Each state is identified with an ID of type String. All states can be completely different but they should have the same internal date.
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	=== Create propagator from FirstOrderIntegrator ===		=== Create propagator from FirstOrderIntegrator ===

	The [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/numerical/multi/MultiNumericalPropagator.html MultiNumericalPropagator] should be created by giving a [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/math/ode/FirstOrderIntegrator.html FirstOrderIntegrator].		The [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/numerical/multi/MultiNumericalPropagator.html MultiNumericalPropagator] should be created by giving a [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/math/ode/FirstOrderIntegrator.html FirstOrderIntegrator].

	<code>final MultiNumericalPropagator propagator = new MultiNumericalPropagator(integrator);</code>		<code>final MultiNumericalPropagator propagator = new MultiNumericalPropagator(integrator);</code>
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	=== Add additional equations ===		=== Add additional equations ===
	As for the [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/numerical/NumericalPropagator.html NumericalPropagator], additional equations corresponding to the additional states of each states should be added to the propagator.		As for the [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/numerical/NumericalPropagator.html NumericalPropagator], additional equations corresponding to the additional states of each states should be added to the propagator.

	These additional equations are given to the multi numerical propagator for a specific state thanks to the following methods :		These additional equations are given to the multi numerical propagator for a specific state thanks to the following methods :
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	=== Propagate the attitude ===		=== Propagate the attitude ===

	As for the [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/numerical/NumericalPropagator.html NumericalPropagator], to propagate the [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/attitudes/Attitude.html Attitude] of a specific state, two treatments could be applied :		As for the [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/numerical/NumericalPropagator.html NumericalPropagator], to propagate the [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/attitudes/Attitude.html Attitude] of a specific state, two treatments could be applied :

	*compute the attitude with an [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/attitudes/AttitudeProvider.html AttitudeProvider] : '''''setAttitudeProvider(AttitudeProvider, String)'''''.<br>It is possible to deals with :		*compute the attitude with an [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/attitudes/AttitudeProvider.html AttitudeProvider] : '''''setAttitudeProvider(AttitudeProvider, String)'''''.<br>It is possible to deals with :
	**a single attitude by calling '''''setAttitudeProvider(AttitudeProvider, String)'''''		**a single attitude by calling '''''setAttitudeProvider(AttitudeProvider, String)'''''
	**two attitudes by calling '''''setAttitudeProviderForces(AttitudeProvider, String)''''' or '''''setAttitudeProviderEvents(AttitudeProvider, String)'''''. It is not possible to call '''''setAttitudeProvider(AttitudeProvider, String)''''' and '''''setAttitudeProviderForces(AttitudeProvider, String)''''' (or '''''setAttitudeProviderEvents(AttitudeProvider, String)''''')		**two attitudes by calling '''''setAttitudeProviderForces(AttitudeProvider, String)''''' or '''''setAttitudeProviderEvents(AttitudeProvider, String)'''''. It is not possible to call '''''setAttitudeProvider(AttitudeProvider, String)''''' and '''''setAttitudeProviderForces(AttitudeProvider, String)''''' (or '''''setAttitudeProviderEvents(AttitudeProvider, String)''''')
	*propagate the attitude as a 7-dimension additional state : '''''addAttitudeEquation(AttitudeEquation, String)'''''.<br>In practical terms, the user has to build the additional equation by extending the abstract class [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/numerical/AttitudeEquation.html AttitudeEquation], call '''''addAttitudeEquation(AttitudeEquation, String)'''''.		*propagate the attitude as a 7-dimension additional state : '''''addAttitudeEquation(AttitudeEquation, String)'''''.<br>In practical terms, the user has to build the additional equation by extending the abstract class [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/numerical/AttitudeEquation.html AttitudeEquation], call '''''addAttitudeEquation(AttitudeEquation, String)'''''.

	See [ORB_PRO_UseP mono numerical propagation] chapter for more details.		See [ORB_PRO_UseP mono numerical propagation] chapter for more details.
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	=== Add event detector ===		=== Add event detector ===
	The user could add :		The user could add :
	*an [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/events/EventDetector.html EventDetector] associated with a specific state using '''''addEventDetector(EventDetector, String)'''''		*an [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/events/EventDetector.html EventDetector] associated with a specific state using '''''addEventDetector(EventDetector, String)'''''
	*a [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/events/multi/MultiEventDetector.html MultiEventDetector] associated with several states added to the propagator using '''''addEventDetector(MultiEventDetector)'''''		*a [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/events/multi/MultiEventDetector.html MultiEventDetector] associated with several states added to the propagator using '''''addEventDetector(MultiEventDetector)'''''

	See [MIS_EVT_Home events presentation] and [MIS_MEVEN_Home multi events presentation] chapters for more details.		See [MIS_EVT_Home events presentation] and [MIS_MEVEN_Home multi events presentation] chapters for more details.

User Manual 4.0 Multi Propagation - Historique des versions

Admin le 21 février 2018 à 14:24

Admin : /* Contents */

Admin : /* Javadoc */

Admin le 19 février 2018 à 16:36

Admin : /* Add event detector */

Admin : /* Set the central attraction coefficient */

Admin : /* Propagate the attitude */

Admin : /* Add additional equations */

Admin : /* Add additional equations */

Admin : /* Add initial states */

Admin : /* Contents */

Admin : /* Javadoc */

Admin : /* Add event detector */

Admin : /* Set the central attraction coefficient */

Admin : /* Propagate the attitude */

Admin : /* Add additional equations */

Admin : /* Add additional equations */

Admin : /* Add initial states */