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Analysis of Full Order Observer Based Control for Spacecraft Orbit Maneuver Trajectory Under Solar Radiation Pressure

Fuente: arXiv

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Dettagli Bibliografici
Autore principale:	Zhang, Haoyang
Natura:	Preprint
Pubblicazione:	2026
Soggetti:	Systems and Control
Accesso online:	Acceder al recurso
Tags:	Aggiungi Tag Nessun Tag, puoi essere il primo ad aggiungerne!!

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