User Manual 4.0 Analytical propagation - Historique des versions

Admin : /* J2 secular propagator */

2020-09-21T15:12:39Z

J2 secular propagator

← Version précédente		Version du 21 septembre 2020 à 15:12
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	'''Warning''': if the frame in which model coefficients are expressed is not inertial (ex: TIRF or ITRF), then an exception is thrown.		'''Warning''': if the frame in which model coefficients are expressed is not inertial (ex: TIRF or ITRF), then an exception is thrown.

	Note that J2 transition matrix can be retrieved through method <~~syntaxhighlight lang="java"~~>getTransitionMatrix</~~syntaxhighlight~~> of J2 propagator.		Note that J2 transition matrix can be retrieved through method <code>getTransitionMatrix</code> of J2 propagator.

	=== Lyddane propagators ===		=== Lyddane propagators ===

Admin : /* J2 secular propagator */

2020-09-21T15:11:53Z

J2 secular propagator

← Version précédente		Version du 21 septembre 2020 à 15:11
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	'''Warning''': if the frame in which model coefficients are expressed is not inertial (ex: TIRF or ITRF), then an exception is thrown.		'''Warning''': if the frame in which model coefficients are expressed is not inertial (ex: TIRF or ITRF), then an exception is thrown.

			Note that J2 transition matrix can be retrieved through method <syntaxhighlight lang="java">getTransitionMatrix</syntaxhighlight> of J2 propagator.

	=== Lyddane propagators ===		=== Lyddane propagators ===

Admin le 28 février 2018 à 08:39

2018-02-28T08:39:45Z

← Version précédente		Version du 28 février 2018 à 08:39
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	'''Warning''': Used algorithm for osculating to mean conversion often consists in an iterative algorithm with a convergence criterion. As a result convergence is not always ensured, depending on the underlying theory. Static method <code>setThreshold()</code> allows the user to change the convergence threshold if convergence issues arise.		'''Warning''': Used algorithm for osculating to mean conversion often consists in an iterative algorithm with a convergence criterion. As a result convergence is not always ensured, depending on the underlying theory. Static method <code>setThreshold()</code> allows the user to change the convergence threshold if convergence issues arise.
	Example of convergence issues: Lyddane propagators fails to return mean elements from the following Keplerian osculating elements: [a = 24400km, e = 0.72, i = 0 deg, gom = 0 deg, pom = 0 deg, M = 0.1 deg].		Example of convergence issues: Lyddane propagators fails to return mean elements from the following Keplerian osculating elements: [a = 24400km, e = 0.72, i = 0 deg, gom = 0 deg, pom = 0 deg, M = 0.1 deg].

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

	== Getting Started ==		== Getting Started ==
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	\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/PVCoordinatePropagator.html ...]		\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/PVCoordinatePropagator.html ...]
	\|}		\|}


			[[Category:User_Manual_4.0_Orbit_Propagation]]

Admin : /* Classes */

2018-02-21T16:44:11Z

Classes

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 === Classes ===
-|=(% colspan="3" %)Class|=(% colspan="6" %)Summary|=(% colspan="1" %)Javadoc
+{| class="wikitable"
-|(% colspan="3" %)'''AbstractPropagator'''|(% colspan="6" %)Common handling of Propagator methods for analytical propagators.|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/AbstractPropagator.html ...]
+|-
-|(% 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" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/SpacecraftState.html ...]
+! scope="col"| Class
-|(% colspan="3" %)'''TLE'''|(% colspan="6" %)This class is a container for a single set of TLE data.|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/tle/TLE.html ...]
+! scope="col"| Summary
-|(% colspan="3" %)'''KeplerianPropagator'''|(% colspan="6" %)Simple keplerian orbit propagator.|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/KeplerianPropagator.html ...]
+! scope="col"| Javadoc
-|(% colspan="3" %)'''EcksteinHechlerPropagator'''|(% colspan="6" %)This class propagates a SpacecraftState  using the analytical Eckstein-Hechler model.|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/EcksteinHechlerPropagator.html ...]
+|-
-|(% colspan="3" %)'''J2SecularPropagator'''|(% colspan="6" %)This class propagates a SpacecraftState  using the analytical J2 secular model.|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/J2SecularPropagator.html ...]
+|'''AbstractPropagator'''
-|(% colspan="3" %)'''LyddaneSecularPropagator'''|(% colspan="6" %)This class propagates a SpacecraftState  using the analytical Lyddane secular model.|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/LyddaneSecularPropagator.html ...]
+|Common handling of Propagator methods for analytical propagators.
-|(% colspan="3" %)'''LyddaneLongPeriodPropagator'''|(% colspan="6" %)This class propagates a SpacecraftState  using the analytical Lyddane secular + long period model.|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/LyddaneLongPeriodPropagator.html ...]
+|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/AbstractPropagator.html ...]
-|(% colspan="3" %)'''Analytical2DParameterModel'''|(% colspan="6" %)This class represent an orbital parameter model to use with a Analytical2DPropagator|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/twod/Analytical2DParameterModel.html ...]
+|-
-|(% colspan="3" %)'''Analytical2DOrbitModel'''|(% colspan="6" %)This class represent an orbit model to use with a Analytical2DPropagator|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/twod/Analytical2DOrbitModel.html ...]
+|'''SpacecraftState'''
-|(% colspan="3" %)'''Analytical2DPropagator'''|(% colspan="6" %)This class represents a 2D propagator.|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/twod/Analytical2DPropagator.html ...]
+|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="3" %)'''TLEPropagator'''|(% colspan="6" %)This class provides elements to propagate TLE's.|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/tle/TLEPropagator.html ...]
+|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/SpacecraftState.html ...]
-|(% colspan="3" %)'''Ephemeris'''|(% colspan="6" %)This class is designed to accept and handle tabulated orbital entries. Tabulated entries are classified and then extrapolated in way to obtain continuous output, with accuracy and computation methods configured by the user.|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/precomputed/Ephemeris.html ...]
+|-
-|(% colspan="3" %)'''EphemerisPvLagrange'''|(% colspan="6" %)This class handles tabulated spacecraft states entries and implements PVCoordinatesProvider interface. Tabulated entries are chronologically classified. A Lagrange interpolation is perfomed to compute PV coordinates at a given date.|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/orbits/pvcoordinates/EphemerisPvLagrange.html ...]
+|'''TLE'''
-|(% colspan="3" %)'''EphemerisPvHermite'''|(% colspan="6" %)This class handles tabulated spacecraft states entries and implements PVCoordinatesProvider interface. Tabulated entries are chronologically classified. A Hermite interpolation is perfomed to compute PV coordinates at a given date.|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/orbits/pvcoordinates/EphemerisPvHermite.html ...]
+|This class is a container for a single set of TLE data.
-| and '''EphemerisPvHermite'''. |(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/PVCoordinatePropagator.html ...]
+|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/tle/TLE.html ...]

Admin : /* Interfaces */

2018-02-21T16:40:01Z

Interfaces

← Version précédente		Version du 21 février 2018 à 16:40
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	! scope="col"\| Javadoc		! scope="col"\| Javadoc
	\|-		\|-
	\|**Propagator		\|'''Propagator'''
	\|This interface provides a way to propagate an orbit at any time.		\|This interface provides a way to propagate an orbit at any time.
	\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/Propagator.html ...]		\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/Propagator.html ...]
	\|-		\|-
	\|**MeanOsculatingElementsProvider		\|'''MeanOsculatingElementsProvider'''
	\|This interface provides mean <=> osculating elements conversion.		\|This interface provides mean <=> osculating elements conversion.
	\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/MeanOsculatingElementsProvider.html ...]		\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/MeanOsculatingElementsProvider.html ...]

Admin le 21 février 2018 à 14:20

2018-02-21T14:20:57Z

Admin : /* Contents */

2018-02-21T09:36:44Z

Contents

← Version précédente		Version du 21 février 2018 à 09:36
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	== Contents ==		== Contents ==
	=== Interfaces ===		=== Interfaces ===
	\|=~~(% colspan~~="3" %)Interface~~\|=(% colspan~~="6" %)Summary~~\|=(% colspan~~="1" %)Javadoc		{\| class="wikitable"
	\|~~(% colspan="3" %)~~**Propagator\|~~(% colspan="6" %)~~This interface provides a way to propagate an orbit at any time.\|~~(% colspan="1" %)~~[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/Propagator.html ...]		\|-
	\|~~(% colspan="3" %)~~**MeanOsculatingElementsProvider\|~~(% colspan="6" %)~~This interface provides mean <=> osculating elements conversion.\|~~(% colspan="1" %)~~[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/MeanOsculatingElementsProvider.html ...]		! scope="col"\| Interface
			! scope="col"\| Summary
			! scope="col"\| Javadoc
			\|-
			\|**Propagator
			\|This interface provides a way to propagate an orbit at any time.
			\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/Propagator.html ...]
			\|-
			\|**MeanOsculatingElementsProvider
			\|This interface provides mean <=> osculating elements conversion.
			\|[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/MeanOsculatingElementsProvider.html ...]
			\|}

	=== Classes ===		=== Classes ===

Admin : /* Javadoc */

2018-02-21T09:33:33Z

Javadoc

← Version précédente		Version du 21 février 2018 à 09:33
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	=== Javadoc ===		=== Javadoc ===
	Some of the propagation packages available in the Patrius library are listed here :		Some of the propagation packages available in the Patrius library are listed here :


	{\| class="wikitable"		{\| class="wikitable"

Admin : /* Introduction */

2018-02-21T09:33:23Z

Introduction

← Version précédente		Version du 21 février 2018 à 09:33
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	Some of the propagation packages available in the Patrius library are listed here :		Some of the propagation packages available in the Patrius library are listed here :

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

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

Admin : Admin a déplacé la page Analytical propagation vers User Manual 4.0 Analytical propagation sans laisser de redirection

2018-02-19T14:27:52Z

Admin a déplacé la page Analytical propagation vers User Manual 4.0 Analytical propagation sans laisser de redirection

← Version précédente		Version du 19 février 2018 à 14:27
(Aucune différence)

← Version précédente		Version du 21 février 2018 à 14:20
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	== Introduction ==		== Introduction ==
	=== Scope ===		=== Scope ===
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	== Features Description ==		== Features Description ==

	Analytical propagators can be defined without any [{{~~PathCurrentJavaDoc~~}}//fr/cnes/sirius/patrius/attitudes/AttitudeProvider.html AttitudeProvider].		Analytical propagators can be defined without any [{{JavaDoc4.0}}//fr/cnes/sirius/patrius/attitudes/AttitudeProvider.html AttitudeProvider].
	<syntaxhighlight lang="java">		<syntaxhighlight lang="java">
	KeplerianPropagator extrapolator = new KeplerianPropagator(initialOrbit);		KeplerianPropagator extrapolator = new KeplerianPropagator(initialOrbit);
Ligne 226 :		Ligne 224 :

	==== The "centered" part ====		==== The "centered" part ====
	The "centered" part is any function having one variable : the date. It is represented by an object of type [{{~~PathCurrentJavaDoc~~}}//fr/cnes/sirius/patrius/propagation/analytical/twod/UnivariateDateFunction.html UnivariateDateFunction]. <br>		The "centered" part is any function having one variable : the date. It is represented by an object of type [{{JavaDoc4.0}}//fr/cnes/sirius/patrius/propagation/analytical/twod/UnivariateDateFunction.html UnivariateDateFunction]. <br>
	At this time, the following univariate functions are available :		At this time, the following univariate functions are available :
	* piecewise functions of date which are reprensented by the extensions of [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/analytical/twod/AbstractDateIntervalFunction.html AbstractDateIntervalFunction] :		* piecewise functions of date which are reprensented by the extensions of [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/twod/AbstractDateIntervalFunction.html AbstractDateIntervalFunction] :
	** [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/analytical/twod/DateIntervalLinearFunction.html piecewise linear functions of date]		** [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/twod/DateIntervalLinearFunction.html piecewise linear functions of date]
	** [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/analytical/twod/DateIntervalParabolicFunction.html piecewise 2nd order polynomial functions of date]		** [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/twod/DateIntervalParabolicFunction.html piecewise 2nd order polynomial functions of date]
	* [{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/analytical/twod/DatePolynomialFunction.html polynomial functions of date]		* [{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/twod/DatePolynomialFunction.html polynomial functions of date]
	[[File:Analytical2DPropagatorCenteredFunction.png\|center]]		[[File:Analytical2DPropagatorCenteredFunction.png\|center]]

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	=== Classes ===		=== Classes ===
	\|=(% colspan="3" %)Class\|=(% colspan="6" %)Summary\|=(% colspan="1" %)Javadoc		\|=(% colspan="3" %)Class\|=(% colspan="6" %)Summary\|=(% colspan="1" %)Javadoc
	\|(% colspan="3" %)'''AbstractPropagator'''\|(% colspan="6" %)Common handling of Propagator methods for analytical propagators.\|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/AbstractPropagator.html ...]		\|(% colspan="3" %)'''AbstractPropagator'''\|(% colspan="6" %)Common handling of Propagator methods for analytical propagators.\|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/AbstractPropagator.html ...]
	\|(% 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" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/SpacecraftState.html ...]		\|(% 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" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/SpacecraftState.html ...]
	\|(% colspan="3" %)'''TLE'''\|(% colspan="6" %)This class is a container for a single set of TLE data.\|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/analytical/tle/TLE.html ...]		\|(% colspan="3" %)'''TLE'''\|(% colspan="6" %)This class is a container for a single set of TLE data.\|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/tle/TLE.html ...]
	\|(% colspan="3" %)'''KeplerianPropagator'''\|(% colspan="6" %)Simple keplerian orbit propagator.\|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/analytical/KeplerianPropagator.html ...]		\|(% colspan="3" %)'''KeplerianPropagator'''\|(% colspan="6" %)Simple keplerian orbit propagator.\|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/KeplerianPropagator.html ...]
	\|(% colspan="3" %)'''EcksteinHechlerPropagator'''\|(% colspan="6" %)This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.\|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/analytical/EcksteinHechlerPropagator.html ...]		\|(% colspan="3" %)'''EcksteinHechlerPropagator'''\|(% colspan="6" %)This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.\|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/EcksteinHechlerPropagator.html ...]
	\|(% colspan="3" %)'''J2SecularPropagator'''\|(% colspan="6" %)This class propagates a SpacecraftState using the analytical J2 secular model.\|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/analytical/J2SecularPropagator.html ...]		\|(% colspan="3" %)'''J2SecularPropagator'''\|(% colspan="6" %)This class propagates a SpacecraftState using the analytical J2 secular model.\|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/J2SecularPropagator.html ...]
	\|(% colspan="3" %)'''LyddaneSecularPropagator'''\|(% colspan="6" %)This class propagates a SpacecraftState using the analytical Lyddane secular model.\|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/analytical/LyddaneSecularPropagator.html ...]		\|(% colspan="3" %)'''LyddaneSecularPropagator'''\|(% colspan="6" %)This class propagates a SpacecraftState using the analytical Lyddane secular model.\|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/LyddaneSecularPropagator.html ...]
	\|(% colspan="3" %)'''LyddaneLongPeriodPropagator'''\|(% colspan="6" %)This class propagates a SpacecraftState using the analytical Lyddane secular + long period model.\|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/analytical/LyddaneLongPeriodPropagator.html ...]		\|(% colspan="3" %)'''LyddaneLongPeriodPropagator'''\|(% colspan="6" %)This class propagates a SpacecraftState using the analytical Lyddane secular + long period model.\|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/LyddaneLongPeriodPropagator.html ...]
	\|(% colspan="3" %)'''Analytical2DParameterModel'''\|(% colspan="6" %)This class represent an orbital parameter model to use with a Analytical2DPropagator\|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/analytical/twod/Analytical2DParameterModel.html ...]		\|(% colspan="3" %)'''Analytical2DParameterModel'''\|(% colspan="6" %)This class represent an orbital parameter model to use with a Analytical2DPropagator\|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/twod/Analytical2DParameterModel.html ...]
	\|(% colspan="3" %)'''Analytical2DOrbitModel'''\|(% colspan="6" %)This class represent an orbit model to use with a Analytical2DPropagator\|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/analytical/twod/Analytical2DOrbitModel.html ...]		\|(% colspan="3" %)'''Analytical2DOrbitModel'''\|(% colspan="6" %)This class represent an orbit model to use with a Analytical2DPropagator\|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/twod/Analytical2DOrbitModel.html ...]
	\|(% colspan="3" %)'''Analytical2DPropagator'''\|(% colspan="6" %)This class represents a 2D propagator.\|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/analytical/twod/Analytical2DPropagator.html ...]		\|(% colspan="3" %)'''Analytical2DPropagator'''\|(% colspan="6" %)This class represents a 2D propagator.\|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/twod/Analytical2DPropagator.html ...]
	\|(% colspan="3" %)'''TLEPropagator'''\|(% colspan="6" %)This class provides elements to propagate TLE's.\|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/analytical/tle/TLEPropagator.html ...]		\|(% colspan="3" %)'''TLEPropagator'''\|(% colspan="6" %)This class provides elements to propagate TLE's.\|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/analytical/tle/TLEPropagator.html ...]
	\|(% colspan="3" %)'''Ephemeris'''\|(% colspan="6" %)This class is designed to accept and handle tabulated orbital entries. Tabulated entries are classified and then extrapolated in way to obtain continuous output, with accuracy and computation methods configured by the user.\|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/precomputed/Ephemeris.html ...]		\|(% colspan="3" %)'''Ephemeris'''\|(% colspan="6" %)This class is designed to accept and handle tabulated orbital entries. Tabulated entries are classified and then extrapolated in way to obtain continuous output, with accuracy and computation methods configured by the user.\|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/precomputed/Ephemeris.html ...]
	\|(% colspan="3" %)'''EphemerisPvLagrange'''\|(% colspan="6" %)This class handles tabulated spacecraft states entries and implements PVCoordinatesProvider interface. Tabulated entries are chronologically classified. A Lagrange interpolation is perfomed to compute PV coordinates at a given date.\|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/orbits/pvcoordinates/EphemerisPvLagrange.html ...]		\|(% colspan="3" %)'''EphemerisPvLagrange'''\|(% colspan="6" %)This class handles tabulated spacecraft states entries and implements PVCoordinatesProvider interface. Tabulated entries are chronologically classified. A Lagrange interpolation is perfomed to compute PV coordinates at a given date.\|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/orbits/pvcoordinates/EphemerisPvLagrange.html ...]
	\|(% colspan="3" %)'''EphemerisPvHermite'''\|(% colspan="6" %)This class handles tabulated spacecraft states entries and implements PVCoordinatesProvider interface. Tabulated entries are chronologically classified. A Hermite interpolation is perfomed to compute PV coordinates at a given date.\|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/orbits/pvcoordinates/EphemerisPvHermite.html ...]		\|(% colspan="3" %)'''EphemerisPvHermite'''\|(% colspan="6" %)This class handles tabulated spacecraft states entries and implements PVCoordinatesProvider interface. Tabulated entries are chronologically classified. A Hermite interpolation is perfomed to compute PV coordinates at a given date.\|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/orbits/pvcoordinates/EphemerisPvHermite.html ...]
	\| and '''EphemerisPvHermite'''. \|(% colspan="1" %)[{{~~PathCurrentJavaDoc~~}}/fr/cnes/sirius/patrius/propagation/PVCoordinatePropagator.html ...]		\| and '''EphemerisPvHermite'''. \|(% colspan="1" %)[{{JavaDoc4.0}}/fr/cnes/sirius/patrius/propagation/PVCoordinatePropagator.html ...]

User Manual 4.0 Analytical propagation - Historique des versions

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