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Rigid body equations of motion for modeling and control of spacecraft formations - Part 1: absolute equations of motion

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dc.contributor.author Ploen, Scott R.
dc.contributor.author Hadaegh, Fred Y.
dc.contributor.author Scharf, Daniel P.
dc.date.accessioned 2005-11-07T23:27:12Z
dc.date.available 2005-11-07T23:27:12Z
dc.date.issued 2004-06
dc.identifier.citation 2004 American Control Conference, Boston, MA, June 30, 2004 en
dc.identifier.clearanceno 04-0669
dc.identifier.uri http://hdl.handle.net/2014/37881
dc.description.abstract In this paper, we present a tensorial derivation of the equations of motion of a formation consisting of N spacecraft each modeled as a rigid body. en
dc.description.sponsorship NASA en
dc.format.extent 708893 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004. en
dc.subject formation flying en
dc.title Rigid body equations of motion for modeling and control of spacecraft formations - Part 1: absolute equations of motion en
dc.type Preprint en


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