Fully actuated system approach for spacecraft rendezvous system with actuator saturation
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DOI: 10.1080/00207721.2024.2317349
Abstract: This paper explores the application of a fully actuated system (FAS) approach to a spacecraft rendezvous system with actuator saturation. A FAS model for the spacecraft rendezvous system is developed, followed by the design of… read more here.
Keywords: system; rendezvous system; fully actuated; approach ... See more keywords