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Orbital Targeting Using Reduced Eccentric Anomaly Low-Thrust Coefficients
dc.contributor.authorHudson, Jennifer S.en_US
dc.contributor.authorScheeres, Daniel J.en_US
dc.date.accessioned2012-04-05T20:35:07Z
dc.date.available2012-04-05T20:35:07Z
dc.date.issued2011en_US
dc.identifier.citationHudson, Jennifer; Scheeres, Daniel (2011). "Orbital Targeting Using Reduced Eccentric Anomaly Low-Thrust Coefficients." Journal of Guidance, Control, and Dynamics, vol. 34 no. 3 (820-831). <http://hdl.handle.net/2027.42/90625>en_US
dc.identifier.issn0731-5090en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/90625
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleOrbital Targeting Using Reduced Eccentric Anomaly Low-Thrust Coefficientsen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationotherUniversity of Michigan; University of Coloradoen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/90625/1/AIAA-51336-469.pdf
dc.identifier.doi10.2514/1.51336en_US
dc.identifier.sourceJournal of Guidance, Control, and Dynamicsen_US
dc.owningcollnameAerospace Engineering, Department of


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