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How do you suggest can I fork this into a modified Goddard problem of having the optimal thrust profile for the rocket to have the maximum time it is on a certain altitude? Are there parts of the code I should focus into?
The text was updated successfully, but these errors were encountered:
How do you suggest can I fork this into a modified Goddard problem of having the optimal thrust profile for the rocket to have the maximum time it is on a certain altitude? Are there parts of the code I should focus into?
The text was updated successfully, but these errors were encountered: