CelestLab is a library of space flight dynamics functions written in Scilab.
This library has been developed by CNES (Centre National d’Etudes Spatiales)
for mission analysis purposes. It is 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...).
But if you would like to report bugs, please go to: http://forge.scilab.org