Currently I am working on a code that optimizes the flight path of an ascending rocket to a final orbit in terms of mass reduction. More precisely I would like my code to optimize my Equations of Motions so that it returns me a function alpha(t). Alpha(t) is a thrust vector control variable.
Which Optimizer should I use for that problem and why?
Hope you can help me out, thanks!

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Mayank Saneja
Mayank Saneja 2022 年 5 月 30 日
Can you please upload your code for the trajectory optimization.
Thank You

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Stephan
Stephan 2018 年 12 月 1 日
編集済み: Stephan 2018 年 12 月 1 日

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Hi,
this appears to be an optimal control problem. Consider to use Symbolic Math Toolbox - espacially have a look at the functionalDerivative function. If you set this expression equal to zero, it enables to get a function alpha(t) that optimizes the functional which describes your system. There are some examples given in the documentation - maybe this is the right choice to tackle your problem.
Best regards
Stephan

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