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ATOMS : CelestLab details
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CelestLab

CNES Space mechanics toolbox for mission analysis
(2395 downloads for this version - 54295 downloads for all versions)
Details
Version
2.3.0
A more recent valid version exists: 3.2.1
Author
CNES - DCT/SB
Owner Organization
CNES - DCT/SB
Maintainers
Thierry Martin
Alain Lamy
Category
License
Creation Date
January 31, 2012
Source created on
Scilab 5.2.x
Binaries available on
Scilab 5.2.x:
Windows 64-bit Windows 32-bit Linux 64-bit Linux 32-bit MacOSX
Install command
--> atomsInstall("celestlab")
Description
            CelestLab is a library of space flight dynamics functions for Scilab. 
This library has been developed by CNES (Centre National d’Etudes Spatiales)
for mission analysis purposes. It can be used for trajectory analysis and orbit
design for various types of missions (around Earth, interplanetary...).  

CelestLab includes about 200 functions that allow mission designers to perform
various tasks such as: orbit propagation, manoeuvre computation, change of
reference frames and coordinates, etc... 

You may leave comments below (any remark, suggestions...). 

For more information about Celestlab: 

- A mailing list has been created. 
To subscribe, send an empty email to: 
celestlab-subscribe@lists.scilab.org
Don't hesitate to use the mailing list if you want to report bugs or make
suggestions. 

- You may also have a look at the news (below). 

            
Files (2)
[1.94 MB]
Source code archive

[3.17 MB]
OS-independent binary for Scilab 5.2.x
Binary version
Automatically generated by the ATOMS compilation chain

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