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5 years ago | |
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| .. | ||
| 2Firm_vfi.jl | 5 years ago | |
| BasicNeuralNet.ipynb | 5 years ago | |
| README.md | 5 years ago | |
| ThoughtsOnUsingPytorch.ipynb | 5 years ago | |
| TransitionDerivatives.ipynb | 5 years ago | |
| TwoFirmVariation.wxmx | 5 years ago | |
| Untitled.ipynb | 5 years ago | |
| composition_Exploration.ipynb | 5 years ago | |
| connect_transition_to_optimality.ipynb | 5 years ago | |
| successful_recursion.ipynb | 5 years ago | |
| test_double.ipynb | 5 years ago | |
README.md
COMPUTATIONAL TODO
Next steps
- implement 'launch function as a function' portion
- This will probably use a neural network as a function type approach.
- substitute the transition functions into the optimality conditions.
- use these optimality conditions to create a loss function
- add boundary conditions to loss function
- get a basic gradient descent/optimization of launch function working.
- add satellite deorbit to model.
- turn this into a framework in a module, not just a single notebook (long term goal)