Main differences between V4.11 and V4.10 : Différence entre versions
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Ligne 16 : | Ligne 16 : | ||
== Bugs fixes == | == Bugs fixes == | ||
− | * | + | * Correction of an anomaly happening while considering a Newtonian gravity model which is not centered on the integration body |
+ | * Correction of the computation of the reference ellipsoid for a FacetBodyShape | ||
+ | * Correction of the LinkType used in the computation of the g function of the SatToSatMutualVisibilityDetector | ||
+ | * Correction of an anomaly happening while evaluation a ForceModel for a SpacecraftState in ITRF | ||
+ | * Correction of the computation of the normal to a OneAxisEllipsoid |
Version du 23 mai 2023 à 09:15
PATRIUS V4.11 is a major release adding some new features and correcting some bugs.
New functionalities
- Circular parameters can now accept hyperbolic orbits
- Broadcast ephemerides model (LNAV and CNAV) for the computation of GNSS trajectories has been added
- Several new detectors have been added
- New class GeodeticTargetDirection to define the direction passing by a GeodeticPoint and a BodyShape
- New class MeteorologicalConditions which encapsulates data about temperature, pressure and humidity
- It is now possible to compute the primitive of a PolynomialFunction and of a ChebyshevPolynomialFunction
- The native frame of a CelestialBody is now the ICRF
- Gravity models are now distinct from the force models (to add a gravity model to the list of force models, the class DirectBodyAttraction should now be used)
- The NumericalPropagator and the MultiNumericalPropagator do not use anymore the Newtonian gravity model by default (it should now be added to the list of the force models)
- The SP3Parser is now capable of reading SP3 files in version "d"
- The new class FacetBodyShapeStatistics allows to compute statistics
- PyramidalField now has a notion of sense of rotation of the field of view (clockwise/counterclockwise)
Bugs fixes
- Correction of an anomaly happening while considering a Newtonian gravity model which is not centered on the integration body
- Correction of the computation of the reference ellipsoid for a FacetBodyShape
- Correction of the LinkType used in the computation of the g function of the SatToSatMutualVisibilityDetector
- Correction of an anomaly happening while evaluation a ForceModel for a SpacecraftState in ITRF
- Correction of the computation of the normal to a OneAxisEllipsoid