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Orbits/CurrentWriting/sections/07_ComputationalApproach.tex

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\documentclass[../Main.tex]{subfiles}
\graphicspath{{\subfix{Assets/img/}}}
\begin{document}
\subsection{Introduction to }
The computational approach I have decided to take is an application of
\cite{MALIAR2018}, where the policy function is approximated using a
neural network.
The approach uses the fact that the euler equation implicitly defines the
optimal policy function, for example:
$[0] = f(x(\theta),\theta)$.
This can easily be turned into a mean square loss function by squaring both
sides,
$0 = f^2(x(\theta),\theta)$,
allowing one to find $x(\dot)$ as the solution to a minimization problem.
By choosing a neural network as the functional approximation, we are able to
take advantage of the significant computational and practical improvements
currently revolutionizing Machine Learning.
In particular, we can now use common frameworks, such as python, PyTorch,
and various online accerators (Google Colab)
which have been optimized for relatively high performance and
straightforward development.
\subsection{Computational Plan}
I have decided to use python and the PyTorch Neural Network library for this project.
The most difficult step is creating the euler equations.
When working with high dimensioned problems involving differentiation,
three general computational approaches exist:
\begin{itemize}
\item Using a symbolic library (sympy) or language (mathematica) to create the
euler equations.
This has the disadvantage of being (very) slow, but the advantage that
for a single problem specification it only needs completed once.
It requires taking a matrix inverse, which can easily complicate formulas,
and is computationally expensive.
\item Using numerical differentiation (ND).
The primary issue with ND is that errors can grow quite quickly when
performing algebra on numerical derivatives.
This requires tracking how errors can grow and compound within your
specific formulation of the problem.
\item Using automatic differentiation (AD) to differentiate the computer code
directly.
This approach has a few major benefits.
\begin{itemize}
\item Precision is high, because you are calcuating symbolic
derivatives of your computer functions.
\item ML is heavily dependent on AD, thus the tools are plentiful
and tested.
\item The coupling of AD and ML lead to a tight integration with
the neural network libraries, simplifying the calibration procedure.
\end{itemize}
\end{itemize}
I have chosen to use the AD to generate a euler equation function, which will
then be the basis of our loss function.
The first step is to construct the intertemporal transition functions
(e.g \ref{put_refs_here}).
%Not sure how much detail to use.
%I'm debating on describing how it is done.
These take derivatives of the value function at time $t$ as an input, and output
derivatives of the value function at time $t+1$.
Once this function has been finished, it can be combined with the laws of motion
in an iterated manner to transition between times $t$ and times $t+k$.
I did so by coding a function that iteratively compose the transition
and laws of motion functions, retuning a $k$-period transition function.
The second step is to generate functions that represent the optimality conditions.
By taking the appropriate derivatives with respect to the laws of motion and
utility functions, this can be constructed explicitly.
Once these two functions are completed, they can be combined to create
the euler equations, as described in appendix \ref{appx??}.
\subsection{Training}
With the euler equation and resulting loss function in place,
standard training approachs can be used to fit the function.
I plan on using some variation on stochastic gradient descent.
Normally, neural networks are trained on real world data.
As this is a synthetic model, I am planning on training it on random selections
from the state space.
If I can data on how satellites are and have been distributed, I plan on
selecting from that distribution.
\subsections{Extensions}
One key question is how to handle the case of heterogeneous agents.
I believe I can address this in the constellation operator's case
by solving for the policy functions of each class of operator
simultaneously.
I still have some questions about this approach and have not dived into
some of the mathemeatics that deeply.
\subsection{Existence concerns}
%check matrix inverses etc.
%
\end{document}