An NMPC scheme that optimizes the reference orbit within a periodic orbit family, with a polynomial model of the family, reduces simulated fuel consumption for cislunar stationkeeping.
A Koopman Operator Tutorial with Othogonal Polynomials
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abstract
The Koopman Operator (KO) offers a promising alternative methodology to solve ordinary differential equations analytically. The solution of the dynamical system is analyzed in terms of observables, which are expressed as a linear combination of the eigenfunctions of the system. Coefficients are evaluated via the Galerkin method, using Legendre polynomials as a set of orthogonal basis functions. This tutorial provides a detailed analysis of the Koopman theory, followed by a rigorous explanation of the KO implementation in a computer environment, where a line-by-line description of a MATLAB code solves the Duffing oscillator application.
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Periodic orbit tracking in cislunar space: A finite-horizon approach
An NMPC scheme that optimizes the reference orbit within a periodic orbit family, with a polynomial model of the family, reduces simulated fuel consumption for cislunar stationkeeping.