2022
DOI: 10.2514/1.g006519
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Dynamics Near the Three-Body Libration Points via Koopman Operator Theory

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Cited by 10 publications
(3 citation statements)
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References 29 publications
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“…A related problem is lunar stationkeeping, namely for Lyapunov and Halo orbits in the circularrestricted three-body problem (CR3BP). One study creatively obtained the Koopman operator approximation of the system matrix through direct computation using Legendre polynomials, which are already by their nature a complete and finite set of orthonormal basis in Hilbert space [15]. See [102] for more information on the CR3BP.…”
Section: Space Systemsmentioning
confidence: 99%
“…A related problem is lunar stationkeeping, namely for Lyapunov and Halo orbits in the circularrestricted three-body problem (CR3BP). One study creatively obtained the Koopman operator approximation of the system matrix through direct computation using Legendre polynomials, which are already by their nature a complete and finite set of orthonormal basis in Hilbert space [15]. See [102] for more information on the CR3BP.…”
Section: Space Systemsmentioning
confidence: 99%
“…84 While the Koopman operator continues to gain popularity, attaining high accuracy frequently involves accounting for the substantial dimensionality of the observables, which, unfortunately, leads to higher computational costs. 82 The development of DAC aims to bridge the gap in utilizing data for practical aerial applications in control systems, ensuring safety and logical operation. It ensures safety by activating only when the primary controller encounters deteriorating conditions, allowing the pilot to decide whether to activate it or not.…”
Section: Introductionmentioning
confidence: 99%
“…In DAC, the Koopman estimator plays a pivotal role in data‐based linearization within the observable space, 79 while the nonlinear control leverages the structural properties of the nonlinear model to enable stability, observability, and performance analysis rigorously. In recent years, the Koopman operator and Koopman linearization successfully have been applied in many aerial and space applications such as low‐thrust trajectory optimization, 80 attitude control of spacecraft, 81 studying the motion of a satellite close to a libration point, 82 approximating analytical solution for Zonal Harmonics problem, 83 and decision making 84 . While the Koopman operator continues to gain popularity, attaining high accuracy frequently involves accounting for the substantial dimensionality of the observables, which, unfortunately, leads to higher computational costs 82 …”
Section: Introductionmentioning
confidence: 99%