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Optimal Plane Changes Using Third-Body Forces
dc.contributor.authorVillac, Benjamin F.en_US
dc.contributor.authorScheeres, Daniel J.en_US
dc.date.accessioned2010-06-01T18:37:00Z
dc.date.available2010-06-01T18:37:00Z
dc.date.issued2004-05en_US
dc.identifier.citationVILLAC, B F; SCHEERES, D J (2004). "Optimal Plane Changes Using Third-Body Forces." Annals of the New York Academy of Sciences 1017(1 Astrodynamics, Space Missions, and Chaos ): 255-266. <http://hdl.handle.net/2027.42/71818>en_US
dc.identifier.issn0077-8923en_US
dc.identifier.issn1749-6632en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/71818
dc.identifier.urihttp://www.ncbi.nlm.nih.gov/sites/entrez?cmd=retrieve&db=pubmed&list_uids=15220151&dopt=citationen_US
dc.description.abstractThe fuel optimality of third-body driven plane changes (i.e., plane changes performed by using third-body forces) over one-impulse transfers is investigated numerically and analytically. In particular, the range of third-body driven plane changes that are realizable is shown to be restricted and one impulse must be used in the uncovered regions. However, when third-body driven plane changes are realizable, it is shown that they are always optimal above a certain critical value (about 40°) that depends on the initial condition. Contour plots of optimal δ V values to perform a desired plane changes are given.en_US
dc.format.extent807949 bytes
dc.format.extent3109 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypetext/plain
dc.publisherBlackwell Publishing Ltden_US
dc.rights2004 New York Academy of Sciencesen_US
dc.subject.otherPlane Change Maneuversen_US
dc.subject.otherThird-body Dynamicsen_US
dc.subject.otherHill's Problemen_US
dc.titleOptimal Plane Changes Using Third-Body Forcesen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelScience (General)en_US
dc.subject.hlbtoplevelScienceen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumDepartment of Aerospace Engineering, The University of Michigan, Ann Arbor, Michigan, USAen_US
dc.identifier.pmid15220151en_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/71818/1/annals.1311.015.pdf
dc.identifier.doi10.1196/annals.1311.015en_US
dc.identifier.sourceAnnals of the New York Academy of Sciencesen_US
dc.identifier.citedreference1 Chobotov, V.A., Ed. 1996. Orbital Mechanics, 2nd edit. AIAA Education Series.en_US
dc.identifier.citedreference2 Villac, B.F., D.J. Scheeres, L.A. D'Amario & M.D. Gumann. 2001. The effect of tidal forces in orbit transfers. Proceedings AAS/AIAA Spaceflight Mechanics Meeting, Santa Barbara, CA.en_US
dc.identifier.citedreferenceVillac, B.F., & D.J. Scheeres. 2003. New class of optimal plane change maneuvers. J. Guid. Control Dynam. 26 ( 5 ): 750 – 757.en_US
dc.identifier.citedreferenceScheeres, D.J., M.D. Guman & B. Villac. 2001. Stability analysis of planetary satellite orbiters: application to the Europa Orbiter. J. Guid. Control Dynam. 24 ( 4 ): 778 – 787.en_US
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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