Main differences between V11.5 and V11.6.2 : Différence entre versions
(→Events logs improvements) |
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| Ligne 9 : | Ligne 9 : | ||
== Events logs improvements == | == Events logs improvements == | ||
| − | Logs for events are improved as all the events are taken into account and not only the ones defines in the [Event Event panel]: | + | Logs for events are improved as all the events are taken into account and not only the ones defines in the [[Event|Event panel]]: |
* First and last point | * First and last point | ||
| Ligne 17 : | Ligne 17 : | ||
== Orbit file as output == | == Orbit file as output == | ||
| − | There is now the possibility to store the final orbit parameters in a specific file. These parameters will be cartesian ones in the inertial output frame defined in [[Output|Output]] | + | There is now the possibility to store the final orbit parameters in a specific file. These parameters will be cartesian ones in the inertial output frame defined in [[Output|Output panel]]. And, of course, this file may be import directly in the '''"Initial Orbit"''' panel ! |
[[File:ImportOrbit.png]] | [[File:ImportOrbit.png]] | ||
Version du 15 décembre 2021 à 13:47
Sommaire
Dependencies
This version uses GENOPUS V2.3.1, GENIUS V1.11.2 and PATRIUS V4.8.
Package names
Package have been renamed to be consistent with other tools. So, they starts with fr.cnes.dynvol.psimu ... When using the GUI mode, no change is visibles but, when using Java interface, an update of the import will be necessary.
Events logs improvements
Logs for events are improved as all the events are taken into account and not only the ones defines in the Event panel:
- First and last point
- start and end of a maneuver (even in case of an impulsive one to see the discontinuity)
- start and end of each attitude change.
Orbit file as output
There is now the possibility to store the final orbit parameters in a specific file. These parameters will be cartesian ones in the inertial output frame defined in Output panel. And, of course, this file may be import directly in the "Initial Orbit" panel !
New EXM and EYM variables
Two new variables have been added corresponding to the components of the mean eccentricity vector: EXM and EYM.
Note also that now, these variables as well as EX and EY (components of the osculating eccentricity vector) corresponds exactly to :
[math]Ex = ecos(w)[/math] and [math]Ey = esin(w)[/math]
... as, previously, these variables was considered as the components for equinoctial parameters.
Complex potential for third bodies
Inline with the new GPForceModels widget from GENOPUS, there is now the possibility to consider complex potential fields for third bodies.
More explicit console output
Console output is more explicit now as described here.
