Main differences between V4.3 and V4.2 : Différence entre versions
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== Bugs fixes == | == Bugs fixes == | ||
* Correction of "Remove detector" feature when propagating several times with the same propagator | * Correction of "Remove detector" feature when propagating several times with the same propagator | ||
| + | * Correction of third body ephemeris through the proper handling of IAU data (TDB scale) | ||
* Correction of event detection: it is now more robust | * Correction of event detection: it is now more robust | ||
| − | * Optimisation of | + | * Optimisation of SpacecraftState handling of attitude for increased performances |
* Optimisation of KinematicsToolkit for increased performance | * Optimisation of KinematicsToolkit for increased performance | ||
* Correction of angle normalization function | * Correction of angle normalization function | ||
Version actuelle en date du 28 mai 2019 à 09:20
PATRIUS V4.3 is a major release adding some new features and correcting some bugs.
New functionalities
- Use of Java 8
- New low-level math frameworks: Math, StrictMath and the fastest library available for each math function
- JAFAMA dependency is now 2.3.1
- Add a possibility to by-pass min step criterion on adaptive stepsize integrators such as DOP853
- Body packages has been refactored (ExtendedOneAxisEllipsoid)
Bugs fixes
- Correction of "Remove detector" feature when propagating several times with the same propagator
- Correction of third body ephemeris through the proper handling of IAU data (TDB scale)
- Correction of event detection: it is now more robust
- Optimisation of SpacecraftState handling of attitude for increased performances
- Optimisation of KinematicsToolkit for increased performance
- Correction of angle normalization function
