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12 lines
528 B
Markdown
12 lines
528 B
Markdown
# COMPUTATIONAL TODO
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## Next steps
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- implement 'launch function as a function' portion
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- This will probably use a neural network as a function type approach.
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- substitute the transition functions into the optimality conditions.
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- use these optimality conditions to create a loss function
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- add boundary conditions to loss function
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- get a basic gradient descent/optimization of launch function working.
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- add satellite deorbit to model.
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- turn this into a framework in a module, not just a single notebook (long term goal)
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