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A formulation of stability for spacecraft formations

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dc.contributor.author Acikmese, Ahmet Behcet
dc.contributor.author Hadaegh, Fred Y.
dc.contributor.author Scharf, Daniel P.
dc.contributor.author Ploen, Scott R.
dc.date.accessioned 2006-07-13T20:47:58Z
dc.date.available 2006-07-13T20:47:58Z
dc.date.issued 2005-06-14
dc.identifier.citation 2006 American Control Conference, Minneapolis, Minnesota, June 14-16, 2005. en
dc.identifier.clearanceno 2006 American Control Conference, Minneapolis, Minnesota, June 14-16, 2005.
dc.identifier.clearanceno 05-2880
dc.identifier.uri http://hdl.handle.net/2014/39505
dc.description.abstract A formulation of stability for a set of spacecraft in formation flight is presented. First, a formation is defined in a precise mathematical form in terms of control interactions. Then, stability is formulated based on input-to-output stability with respect to a partitioning of the formation dynamics. This formulation of stability is shown to be useful in characterizing disturbance propagation in the formation as a function of the partition interconnection topology, and also in analyzing the robustness of sensing, communication, and control topologies. Stability results are presented for hierarchical, cyclic, and disturbance attenuating formations. en
dc.description.sponsorship NASA/JPL en
dc.format.extent 1885924 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2005. en
dc.subject formation flyer en
dc.subject stability en
dc.title A formulation of stability for spacecraft formations en
dc.type Preprint en


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