Decentralized Consensus Control of a Rigid-Body Spacecraft Formation with Communication Delay

Persistent Link:
http://hdl.handle.net/10150/615096
Title:
Decentralized Consensus Control of a Rigid-Body Spacecraft Formation with Communication Delay
Author:
Nazari, Morad; Butcher, Eric A.; Yucelen, Tansel; Sanyal, Amit K.
Affiliation:
University of Arizona; Missouri University of Science and Technology; Syracuse University
Issue Date:
2016-04
Publisher:
American Institute of Aeronautics and Astronautics
Citation:
Decentralized Consensus Control of a Rigid-Body Spacecraft Formation with Communication Delay 2016, 39 (4):838 Journal of Guidance, Control, and Dynamics
Journal:
Journal of Guidance, Control, and Dynamics
Rights:
Copyright © 2015 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
Collection Information:
This item from the UA Faculty Publications collection is made available by the University of Arizona with support from the University of Arizona Libraries. If you have questions, please contact us at repository@u.library.arizona.edu.
Abstract:
The decentralized consensus control of a formation of rigid-body spacecraft is studied in the framework of geometric mechanics while accounting for a constant communication time delay between spacecraft. The relative position and attitude (relative pose) are represented on the Lie group SE(3) and the communication topology is modeled as a digraph. The consensus problem is converted into a local stabilization problem of the error dynamics associated with the Lie algebra se(3) in the form of linear time-invariant delay differential equations with a single discrete delay in the case of a circular orbit, whereas it is in the form of linear time-periodic delay differential equations in the case of an elliptic orbit, in which the stability may be assessed using infinite-dimensional Floquet theory. The proposed technique is applied to the consensus control of four spacecraft in the vicinity of a Molniya orbit.
ISSN:
0731-5090; 1533-3884
DOI:
10.2514/1.G001396
Keywords:
decentralized consensus control; multiagent systems; spacecraft formation; communication delay
Version:
Final accepted manuscript
Additional Links:
http://arc.aiaa.org/doi/10.2514/1.G001396

Full metadata record

DC FieldValue Language
dc.contributor.authorNazari, Moraden
dc.contributor.authorButcher, Eric A.en
dc.contributor.authorYucelen, Tanselen
dc.contributor.authorSanyal, Amit K.en
dc.date.accessioned2016-06-29T19:42:54Z-
dc.date.available2016-06-29T19:42:54Z-
dc.date.issued2016-04-
dc.identifier.citationDecentralized Consensus Control of a Rigid-Body Spacecraft Formation with Communication Delay 2016, 39 (4):838 Journal of Guidance, Control, and Dynamicsen
dc.identifier.issn0731-5090-
dc.identifier.issn1533-3884-
dc.identifier.doi10.2514/1.G001396-
dc.identifier.urihttp://hdl.handle.net/10150/615096-
dc.description.abstractThe decentralized consensus control of a formation of rigid-body spacecraft is studied in the framework of geometric mechanics while accounting for a constant communication time delay between spacecraft. The relative position and attitude (relative pose) are represented on the Lie group SE(3) and the communication topology is modeled as a digraph. The consensus problem is converted into a local stabilization problem of the error dynamics associated with the Lie algebra se(3) in the form of linear time-invariant delay differential equations with a single discrete delay in the case of a circular orbit, whereas it is in the form of linear time-periodic delay differential equations in the case of an elliptic orbit, in which the stability may be assessed using infinite-dimensional Floquet theory. The proposed technique is applied to the consensus control of four spacecraft in the vicinity of a Molniya orbit.en
dc.language.isoenen
dc.publisherAmerican Institute of Aeronautics and Astronauticsen
dc.relation.urlhttp://arc.aiaa.org/doi/10.2514/1.G001396en
dc.rightsCopyright © 2015 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.en
dc.subjectdecentralized consensus controlen
dc.subjectmultiagent systemsen
dc.subjectspacecraft formationen
dc.subjectcommunication delayen
dc.titleDecentralized Consensus Control of a Rigid-Body Spacecraft Formation with Communication Delayen
dc.typeArticleen
dc.contributor.departmentUniversity of Arizonaen
dc.contributor.departmentMissouri University of Science and Technologyen
dc.contributor.departmentSyracuse Universityen
dc.identifier.journalJournal of Guidance, Control, and Dynamicsen
dc.description.collectioninformationThis item from the UA Faculty Publications collection is made available by the University of Arizona with support from the University of Arizona Libraries. If you have questions, please contact us at repository@u.library.arizona.edu.en
dc.eprint.versionFinal accepted manuscripten
All Items in UA Campus Repository are protected by copyright, with all rights reserved, unless otherwise indicated.