EML1 Transfer

General help that does not fall into a more specific category

EML1 Transfer

Postby M.delbourg » Fri May 12, 2017 8:30 am

So I am trying to get my satellite in orbit around the EML1 point. I have found an old script that I adapted for my needs but I can't make it work properly.

The problem seems to come from the Propagation of the Apoapsis, the software tells me that: "Solver subsystem exception: Error inverting the Differential Corrector Jacobian; it appears that the variables in the Vary command(s) do not affect the target parameters in the Achieve command(s)". I have tried to make something else vary, but it doesn't work and I just don't understand why these vary don't work because it seems like they should work.

Can someone tell me what's wrong with my mission sequence ?

thank you very much for your time.
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