Main differences between V4.11 and V4.10 : Différence entre versions

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== 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