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10 juin 2026
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N 10:48 | User Manual 4.18 Celestial bodies 2 modifications historique +37 294 [Admin tsn (2×)] | |||
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10:48 (actu | diff) +506 Admin tsn discussion contributions Balise : Éditeur visuel | ||||
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08:55 (actu | diff) +36 788 Admin tsn discussion contributions (Page créée avec « __NOTOC__ == Introduction == === Scope === The celestial bodies are described by their main features : position and geometry. The positions are ephemeris that must be loaded from models, the geometries are created as one axis ellipsoids or facet bodies. The package provides a factory able to create any celestial body of the solar system. === Javadoc === The classes for bodies description are available in the package <code>bodies</code> of Patrius. {| class="wi... ») Balise : Éditeur visuel : basculé | |||
| N 08:58 | User Manual 4.18 Time diffhist +16 418 Admin tsn discussion contributions (Page créée avec « __NOTOC__ == Introduction == === Scope === Despite its current use, time requires careful attention in the description of physical phenomena. Indeed the rate at which time passes has to be accurate in order to guarantee the best physical description of a phenomenon. To that purpose several time scales have been set up and with the introduction of atomic clocks, more accurate time scales have been defined. === Javadoc === The object related with dates and time s... ») | ||||
| N 08:57 | User Manual 4.18 SpacecraftState diffhist +9 582 Admin tsn discussion contributions (Page créée avec « __NOTOC__ == Introduction == === Scope === This section describes the SpacecraftState object. === Javadoc === The object [{{JavaDoc4.18}}//fr/cnes/sirius/patrius/propagation/SpacecraftState.html SpacecraftState] is available in the package <code>fr.cnes.sirius.patrius.propagation</code>. === Links === Here is only described the SpacecraftState structure. Please refer to [ORB_PRO_Home propagation chapter]. === Useful Documents === None as of now. === Overv... ») | ||||
| N 08:57 | User Manual 4.18 Orbits diffhist +5 525 Admin tsn discussion contributions (Page créée avec « __NOTOC__ == Introduction == === Scope === The "orbits" package contains classes to represent the orbital state of a spacecraft at a given time. Several types of orbits are available (cartesian, keplerian, equinoctial...). The jacobian matrix for each orbital parameter / cartesian parameter conversion are also available for their current value. An "Orbit" (implementing "Orbit" class) object is not to be misunderstood with an "Orbital parameters" object (implemen... ») | ||||
| N 08:56 | User Manual 4.18 Orbital parameters diffhist +5 250 Admin tsn discussion contributions (Page créée avec « __NOTOC__ == Introduction == === Scope === The "Orbital parameters" package contains classes to represent the orbital state of a space object. Several types of parameters are available (cartesian, keplerian, equinoctial... with different position angle definitions : true, mean, eccentric). Orbital parameters do not define a date nor a frame. To fully define an orbit, including date and frame, please refer to [FDY_Orbits_Home Orbits]. === Javadoc === The classe... ») | ||||
| N 08:56 | User Manual 4.18 Frames configuration diffhist +25 313 Admin tsn discussion contributions (Page créée avec « __NOTOC__ == Introduction == === Scope === Frames configuration defines the models and data to use for each frame transformation. Several frames configurations are already available in PATRIUS (IERS 2003, IERS 2010, STELA? etc.) but the user may define its own convention. === Javadoc === {| class="wikitable" |- ! scope="col"| Library ! scope="col"| Javadoc |- |Patrius |[{{JavaDoc4.18}}/fr/cnes/sirius/patrius/frames/configuration/package-summary.html Package fr.c... ») | ||||
| N 08:56 | User Manual 4.18 Frames diffhist +17 232 Admin tsn discussion contributions (Page créée avec « __NOTOC__ == Introduction == === Scope === In Patrius, a frame is represented by the class Frame. The different frames are organized as a tree whose root is the ICRF. A frame is defined by a transformation with respect to its parent. A frame factory enables us to build easily some current frames such as GCRF, EME2000, ITRF... Models and data defining transformations between frame is defined in [FDY_FRCON_Home Frames configuration] === Javadoc === The frames are... ») | ||||