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

Ploen, Scott R.; Hadaegh, Fred Y.; Scharf, Daniel P.

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