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CelestLab - CNES Space Mechanics Toolbox for Scilab
Version 3.5.1
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CelestLab is a Scilab toolbox for Space Flight Dynamics.
It has been developed by CNES (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 comes with an extension module called CelestLabX.
The features in CelestLab that require CelestLabX to be installed are
related to:
- STELA: CNES orbit long-term propagation software
- Two Line Elements
- MSIS2000 atmospheric model
Note:
- CelestLab can be used with Scilab versions 5.5.x to 2025.x.x
- The version of CelestLabX that should be used is 3.5.1
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.
Note: binary version has been created using Scilab 6.0.2, but is compatible with
Scilab 2025.0.0.
