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CelestLab - CNES Space Mechanics Toolbox for Scilab
Version 3.1.0
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CelestLab is a Scilab toolbox for Space Flight Dynamics.
It has been developed by CNES-DCT/SB (Centre National d?Etudes Spatiales -
French Space Agency) for mission analysis purposes.
CelestLab can be used for trajectory analysis and orbit
design for various types of space missions.
It allows engineers to perform tasks such as: orbit propagation, attitude
computation, elementary manoeuvre computation, change of coordinate systems,
...
CelestLab now comes with an extension module called CelestLabX.
CelestLabX includes low-level functions that the user is not supposed to call
directly: all user interfaces and documention are provided in CelestLab.
The new features in CelestLab that require CelestLabX to be installed are
related to:
- STELA: CNES orbit long-term propagation software
- Two Line Elements
If CelestLabX is required but has not been installed, error messages will be
generated by the corresponding CelestLab functions.
Note:
- CelestLab alone (without CelestLabX) can be used with Scilab versions >=
5.3.0.
- The version of CelestLabX that should be used (for users who want it) is
3.1.1.
See:
- CelestLabX Atoms page for more details about CelestLabX:
http://atoms.scilab.org/toolboxes/celestlabx
- The detailed changelog in CelestLab menu for more information about what has
changed in CelestLab compared to the previous version.