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Application of discrete mechanics and optimal control to spacecraft in non-keplerian motion around small solar system bodies

  • Prolonged operations close to small solar system bodies require a sophisticated control logic to minimize propellant mass and maximize operational efficiency. A control logic based on Discrete Mechanics and Optimal Control (DMOC) is proposed and applied to both conventionally propelled and solar sail spacecraft operating at an arbitrarily shaped asteroid in the class of Itokawa. As an example, stand-off inertial hovering is considered, recently identified as a challenging part of the Marco Polo mission. The approach is easily extended to stand-off orbits. We show that DMOC is applicable to spacecraft control at small objects, in particular with regard to the fact that the changes in gravity are exploited by the algorithm to optimally control the spacecraft position. Furthermore, we provide some remarks on promising developments.

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Metadaten
Verfasserangaben:M. Gehler, S. Ober-Blöbaum, Bernd DachwaldORCiD
ISBN:978-161567908-9
Titel des übergeordneten Werkes (Englisch):Procceedings of the 60th International Astronautical Congress
Verlag:Elsevier
Verlagsort:Amsterdam
Dokumentart:Konferenzveröffentlichung
Sprache:Englisch
Erscheinungsjahr:2009
Datum der Publikation (Server):11.03.2024
Freies Schlagwort / Tag:Spacecraft
Erste Seite:1360
Letzte Seite:1371
Bemerkung:
60th International Astronautical Congress 2009, IAC 2009; Daejeon; South Korea; 12 October 2009 through 16 October 2009
Link: https://www.scopus.com/record/display.uri?eid=2-s2.0-77953551203&origin=inward&txGid=55a9d77f018557e6d78a7421419a8393
Zugriffsart:bezahl
Fachbereiche und Einrichtungen:FH Aachen / Fachbereich Luft- und Raumfahrttechnik
FH Aachen / IfB - Institut für Bioengineering
FH Aachen / Kommission für Forschung und Entwicklung
collections:Verlag / Elsevier
Lizenz (Deutsch):License LogoCreative Commons - Namensnennung