Multi-Objective Rendezvous Operation Design Using Neural ODEs with Reservoir Computing Architecture for Trajectory Control Laws
Trajectory control laws based on neural ordinary differential equations (ODEs) were proposed by the authors in a previous study. This paper extends the trajectory control laws by integrating a reservoir computing architecture. The addition can significantly reduce the number of design parameters to...
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Published in | 2024 SICE Festival with Annual Conference (SICE FES) pp. 63 - 68 |
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Main Authors | , |
Format | Conference Proceeding |
Language | English |
Published |
The Society of Instrument and Control Engineers - SICE
27.08.2024
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Subjects | |
Online Access | Get full text |
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Abstract | Trajectory control laws based on neural ordinary differential equations (ODEs) were proposed by the authors in a previous study. This paper extends the trajectory control laws by integrating a reservoir computing architecture. The addition can significantly reduce the number of design parameters to be optimized and thus the computational cost of training while maintaining the structure of the control laws. This enhancement allows general-purpose nonlinear optimization algorithms to be used, extending the application of neural ODEs to operation design optimization beyond the design of control laws. This study verifies the effectiveness of the proposed framework by constructing a control law to achieve the target conditions for a rendezvous operation in a low Earth orbit. Multi-objective design taking advantage of reservoir computing is demonstrated by assessing the Pareto optimal front with respect to orbital transfer time and control accuracy. |
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AbstractList | Trajectory control laws based on neural ordinary differential equations (ODEs) were proposed by the authors in a previous study. This paper extends the trajectory control laws by integrating a reservoir computing architecture. The addition can significantly reduce the number of design parameters to be optimized and thus the computational cost of training while maintaining the structure of the control laws. This enhancement allows general-purpose nonlinear optimization algorithms to be used, extending the application of neural ODEs to operation design optimization beyond the design of control laws. This study verifies the effectiveness of the proposed framework by constructing a control law to achieve the target conditions for a rendezvous operation in a low Earth orbit. Multi-objective design taking advantage of reservoir computing is demonstrated by assessing the Pareto optimal front with respect to orbital transfer time and control accuracy. |
Author | Ueda, Satoshi Ogawa, Hideaki |
Author_xml | – sequence: 1 givenname: Satoshi surname: Ueda fullname: Ueda, Satoshi email: ueda.satoshi@jaxa.jp organization: Research and Development Directorate, Japan Aerospace Exploration Agency,Kanagawa,Japan – sequence: 2 givenname: Hideaki surname: Ogawa fullname: Ogawa, Hideaki email: hideaki.ogawa@aero.kyushu-u.ac.jp organization: Graduate School of Engineering, Kyushu University,Fukuoka,Japan |
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Snippet | Trajectory control laws based on neural ordinary differential equations (ODEs) were proposed by the authors in a previous study. This paper extends the... |
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StartPage | 63 |
SubjectTerms | Computer architecture Design optimization Low earth orbit satellites multi-objective design optimization neural ODE Optimization Orbits Ordinary differential equations Reservoir computing System analysis and design Training Trajectory trajectory control |
Title | Multi-Objective Rendezvous Operation Design Using Neural ODEs with Reservoir Computing Architecture for Trajectory Control Laws |
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