Data initialization - Historique des versions

Admin : /* Solar radiative pressure */

2025-10-10T11:59:28Z

Solar radiative pressure

← Version précédente		Version du 10 octobre 2025 à 11:59
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	new ExtendedOneAxisEllipsoid(REQ, FLAT, (CelestialBodyFrame)ITRF, "EARTH");		new ExtendedOneAxisEllipsoid(REQ, FLAT, (CelestialBodyFrame)ITRF, "EARTH");

	SolarRadiationPressureEllipsoid radPres = new SolarRadiationPressureEllipsoid(dRef, pRef, sunBody, EARTH, assembly, 1.);		SolarRadiationPressureEllipsoid radPres = new SolarRadiationPressureEllipsoid(dRef, pRef, sunBody, sunBody.getShape().getEncompassingSphereRadius(), EARTH, assembly, 1.);

	forces.setSolarRadiationPressure(radPres);		forces.setSolarRadiationPressure(radPres);
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	RediffusedRadiativeModel rdm = new RediffusedRadiativeModel(inAlbedo, inIr, coefAlbedo, coefIr, assembly);		RediffusedRadiativeModel rdm = new RediffusedRadiativeModel(inAlbedo, inIr, coefAlbedo, coefIr, assembly);
	RediffusedRadiationPressure reDiff = new RediffusedRadiationPressure(sunBody, GCRF, inCorona, inMeridian, inEmissivityModel, rdm);		RediffusedRadiationPressure reDiff = new RediffusedRadiationPressure(sunBody, (CelestialBodyFrame)GCRF, inCorona, inMeridian, inEmissivityModel, rdm);

	forces.setRediffusedRadiationPressure(reDiff);		forces.setRediffusedRadiationPressure(reDiff);

Admin : /* Solar radiative pressure */

2025-10-10T11:58:02Z

Solar radiative pressure

← Version précédente		Version du 10 octobre 2025 à 11:58
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	final double pRef = 4.5605E-6;		final double pRef = 4.5605E-6;
	final ExtendedOneAxisEllipsoid EARTH =		final ExtendedOneAxisEllipsoid EARTH =
	new ExtendedOneAxisEllipsoid(REQ, FLAT, ITRF, "EARTH");		new ExtendedOneAxisEllipsoid(REQ, FLAT, (CelestialBodyFrame)ITRF, "EARTH");

	SolarRadiationPressureEllipsoid radPres = new SolarRadiationPressureEllipsoid(dRef, pRef, sunBody, EARTH, assembly, 1.);		SolarRadiationPressureEllipsoid radPres = new SolarRadiationPressureEllipsoid(dRef, pRef, sunBody, EARTH, assembly, 1.);

Admin : /* Aerodynamic */

2025-10-10T11:57:39Z

Aerodynamic

← Version précédente		Version du 10 octobre 2025 à 11:57
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	final Frame ITRF = FramesFactory.getITRF();		final Frame ITRF = FramesFactory.getITRF();
	final ExtendedOneAxisEllipsoid EARTH =		final ExtendedOneAxisEllipsoid EARTH =
	new ExtendedOneAxisEllipsoid(REQ, FLAT, ~~FramesFactory.getITRF~~(), "EARTH");		new ExtendedOneAxisEllipsoid(REQ, FLAT, (CelestialBodyFrame)ITRF, "EARTH");

	final Atmosphere atmosphere = new US76(EARTH);		final Atmosphere atmosphere = new US76(EARTH);

Admin : /* Aerodynamic */

2025-10-10T11:57:11Z

Aerodynamic

← Version précédente		Version du 10 octobre 2025 à 11:57
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	final Frame ITRF = FramesFactory.getITRF();		final Frame ITRF = FramesFactory.getITRF();
	final ExtendedOneAxisEllipsoid EARTH =		final ExtendedOneAxisEllipsoid EARTH =
	new ExtendedOneAxisEllipsoid(REQ, FLAT, ~~ITRF~~, "EARTH");		new ExtendedOneAxisEllipsoid(REQ, FLAT, FramesFactory.getITRF(), "EARTH");

	final Atmosphere atmosphere = new US76(EARTH);		final Atmosphere atmosphere = new US76(EARTH);

Admin : /* Earth features */

2025-10-10T11:56:55Z

Earth features

← Version précédente		Version du 10 octobre 2025 à 11:56
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	<syntaxhighlight lang="java">		<syntaxhighlight lang="java">
	final ExtendedOneAxisEllipsoid EARTH =		final ExtendedOneAxisEllipsoid EARTH =
	new ExtendedOneAxisEllipsoid(REQ, FLAT, ~~ITRF~~, "EARTH");		new ExtendedOneAxisEllipsoid(REQ, FLAT, FramesFactory.getITRF(), "EARTH");
	</syntaxhighlight>		</syntaxhighlight>
	:2. A type of enumerates that will propose some pre-defined configurations as:		:2. A type of enumerates that will propose some pre-defined configurations as:

Admin : /* Potential */

2025-10-10T11:55:50Z

Potential

← Version précédente		Version du 10 octobre 2025 à 11:55
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	<syntaxhighlight lang="java">		<syntaxhighlight lang="java">
	// Potential		// Potential
	final ForceModel potential = EarthGravitationalModelFactory.~~getDroziner~~(GravityFieldNames.GRGS, "grim4s4_gr", 8, 8, true);		final ForceModel potential = new DirectBodyAttraction(EarthGravitationalModelFactory.getBalmino(GravityFieldNames.GRGS, "grim4s4_gr", 0, 0, true));

	final ForceModelsData forces = new ForceModelsData(potential, null, null, null, null, null, null, null, null, null, null, null, null, null, null);		final ForceModelsData forces = new ForceModelsData(potential, null, null, null, null, null, null, null, null, null, null, null, null, null, null);

Admin : /* Vehicle */

2020-05-14T17:34:36Z

Vehicle

← Version précédente		Version du 14 mai 2020 à 17:34
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	</syntaxhighlight>		</syntaxhighlight>

	''<font color=#FF0000>'''Note : for CPU time purpose it is recommanded that the frame (GCRF in the previous example), mandatory in the construction of the vehicle, must be exactly the same that the one used for the propagation ~~(limitation due to PATRIUS)~~.'''</font>''		''<font color=#FF0000>'''Note : for CPU time purpose it is recommanded that the frame (GCRF in the previous example), mandatory in the construction of the vehicle, must be exactly the same that the one used for the propagation.'''</font>''

	In the example below, we will then use the <font color=#4169E1>Vehicle</font> class initializing mass and aerodynamic properties (here no engines and no tanks):		In the example below, we will then use the <font color=#4169E1>Vehicle</font> class initializing mass and aerodynamic properties (here no engines and no tanks):

Admin : /* Vehicle */

2020-05-14T17:34:18Z

Vehicle

← Version précédente		Version du 14 mai 2020 à 17:34
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	</syntaxhighlight>		</syntaxhighlight>

	''<font color=#FF0000>'''Note : for CPU time purpose it is recommanded that the frame (GCRF in the previous example), mandatory in the construction of the vehicle must be exactly the same that the one used for the propagation (limitation due to PATRIUS).'''</font>''		''<font color=#FF0000>'''Note : for CPU time purpose it is recommanded that the frame (GCRF in the previous example), mandatory in the construction of the vehicle, must be exactly the same that the one used for the propagation (limitation due to PATRIUS).'''</font>''

	In the example below, we will then use the <font color=#4169E1>Vehicle</font> class initializing mass and aerodynamic properties (here no engines and no tanks):		In the example below, we will then use the <font color=#4169E1>Vehicle</font> class initializing mass and aerodynamic properties (here no engines and no tanks):

Admin : /* Vehicle */

2020-05-14T17:33:59Z

Vehicle

← Version précédente		Version du 14 mai 2020 à 17:33
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	</syntaxhighlight>		</syntaxhighlight>

	''<font color=#FF0000>'''Note : for ~~<title="Central Processing Unit">~~CPU time purpose it is recommanded that the frame (GCRF in the previous example), mandatory in the construction of the vehicle must be exactly the same that the one used for the propagation (limitation due to PATRIUS).'''</font>''		''<font color=#FF0000>'''Note : for CPU time purpose it is recommanded that the frame (GCRF in the previous example), mandatory in the construction of the vehicle must be exactly the same that the one used for the propagation (limitation due to PATRIUS).'''</font>''

	In the example below, we will then use the <font color=#4169E1>Vehicle</font> class initializing mass and aerodynamic properties (here no engines and no tanks):		In the example below, we will then use the <font color=#4169E1>Vehicle</font> class initializing mass and aerodynamic properties (here no engines and no tanks):

Admin : /* Vehicle */

2020-05-14T17:32:44Z

Vehicle

← Version précédente		Version du 14 mai 2020 à 17:32
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	</syntaxhighlight>		</syntaxhighlight>

	''<font color=#FF0000>'''Note : for <~~font color=#FF8C00~~ title="Central Processing Unit">~~CPUfont>~~ time purpose it is recommanded that the frame (GCRF in the previous example), mandatory in the construction of the vehicle must be exactly the same that the one used for the propagation (limitation due to PATRIUS).'''</font>''		''<font color=#FF0000>'''Note : for <title="Central Processing Unit">CPU time purpose it is recommanded that the frame (GCRF in the previous example), mandatory in the construction of the vehicle must be exactly the same that the one used for the propagation (limitation due to PATRIUS).'''</font>''

	In the example below, we will then use the <font color=#4169E1>Vehicle</font> class initializing mass and aerodynamic properties (here no engines and no tanks):		In the example below, we will then use the <font color=#4169E1>Vehicle</font> class initializing mass and aerodynamic properties (here no engines and no tanks):

Data initialization - Historique des versions

Admin : /* Solar radiative pressure */

Admin : /* Solar radiative pressure */

Admin : /* Aerodynamic */

Admin : /* Aerodynamic */

Admin : /* Earth features */

Admin : /* Potential */

Admin : /* Vehicle */

Admin : /* Vehicle */

Admin : /* Vehicle */

Admin : /* Vehicle */

Admin : /* Solar radiative pressure */

Admin : /* Solar radiative pressure */

Admin : /* Aerodynamic */

Admin : /* Aerodynamic */

Admin : /* Earth features */

Admin : /* Potential */

Admin : /* Vehicle */

Admin : /* Vehicle */

Admin : /* Vehicle */

Admin : /* Vehicle */