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Conference Paper: Semi-global stabilization of linear time-delay systems with input energy constraint
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TitleSemi-global stabilization of linear time-delay systems with input energy constraint
 
AuthorsZhou, B3
Lin, Z1
Lam, J2
 
KeywordsActuator delay
Circular orbit
Delay independent
Delay-dependent
Energy constraint
 
Issue Date2011
 
PublisherIFAC.
 
CitationThe 18th World Congress of the International Federation of Automatic Control (IFAC 2011), Milano, Italy, 28 August-2 September 2011. In Proceedings of the 18th IFAC World Congress, 2011, v. 18 pt. 1, p. 5106–5111 [How to Cite?]
DOI: http://dx.doi.org/10.3182/20110828-6-IT-1002.03409
 
AbstractThis paper is concerned with semi-global stabilization of linear systems with actuator delay and energy constraints. Under the condition of null controllability by vanishing energy, the parametric Lyapunov equation based L2 low gain feedback is adopted to solve the problem. If the delay in the system is exactly known, a delay-dependent controller is designed and if the delay in the system is either time-varying or not exactly known, a delay-independent controller is established. The proposed approach is used in the linearized model of the relative motion in the orbit plane of a spacecraft with respect to another in a circular orbit around the Earth to validate its effectiveness. © 2011 IFAC.
 
ISBN978-3-902661-93-7
 
ISSN1474-6670
 
DOIhttp://dx.doi.org/10.3182/20110828-6-IT-1002.03409
 
DC FieldValue
dc.contributor.authorZhou, B
 
dc.contributor.authorLin, Z
 
dc.contributor.authorLam, J
 
dc.date.accessioned2012-09-21T01:43:28Z
 
dc.date.available2012-09-21T01:43:28Z
 
dc.date.issued2011
 
dc.description.abstractThis paper is concerned with semi-global stabilization of linear systems with actuator delay and energy constraints. Under the condition of null controllability by vanishing energy, the parametric Lyapunov equation based L2 low gain feedback is adopted to solve the problem. If the delay in the system is exactly known, a delay-dependent controller is designed and if the delay in the system is either time-varying or not exactly known, a delay-independent controller is established. The proposed approach is used in the linearized model of the relative motion in the orbit plane of a spacecraft with respect to another in a circular orbit around the Earth to validate its effectiveness. © 2011 IFAC.
 
dc.description.naturepostprint
 
dc.description.otherThe 18th World Congress of the International Federation of Automatic Control (IFAC 2011), Milano, Italy, 28 August-2 September 2011. In Proceedings of the 18th IFAC World Congress, 2011, v. 18 pt. 1, p. 5106–5111
 
dc.identifier.citationThe 18th World Congress of the International Federation of Automatic Control (IFAC 2011), Milano, Italy, 28 August-2 September 2011. In Proceedings of the 18th IFAC World Congress, 2011, v. 18 pt. 1, p. 5106–5111 [How to Cite?]
DOI: http://dx.doi.org/10.3182/20110828-6-IT-1002.03409
 
dc.identifier.doihttp://dx.doi.org/10.3182/20110828-6-IT-1002.03409
 
dc.identifier.epage5111
 
dc.identifier.hkuros208813
 
dc.identifier.isbn978-3-902661-93-7
 
dc.identifier.issn1474-6670
 
dc.identifier.issuept. 1
 
dc.identifier.scopuseid_2-s2.0-84866754211
 
dc.identifier.spage5106
 
dc.identifier.urihttp://hdl.handle.net/10722/166894
 
dc.identifier.volume18
 
dc.languageeng
 
dc.publisherIFAC.
 
dc.relation.ispartofProceedings of the 18th IFAC World Congress
 
dc.rightsCreative Commons: Attribution 3.0 Hong Kong License
 
dc.subjectActuator delay
 
dc.subjectCircular orbit
 
dc.subjectDelay independent
 
dc.subjectDelay-dependent
 
dc.subjectEnergy constraint
 
dc.titleSemi-global stabilization of linear time-delay systems with input energy constraint
 
dc.typeConference_Paper
 
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<item><contributor.author>Zhou, B</contributor.author>
<contributor.author>Lin, Z</contributor.author>
<contributor.author>Lam, J</contributor.author>
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<description.abstract>This paper is concerned with semi-global stabilization of linear systems with actuator delay and energy constraints. Under the condition of null controllability by vanishing energy, the parametric Lyapunov equation based L2 low gain feedback is adopted to solve the problem. If the delay in the system is exactly known, a delay-dependent controller is designed and if the delay in the system is either time-varying or not exactly known, a delay-independent controller is established. The proposed approach is used in the linearized model of the relative motion in the orbit plane of a spacecraft with respect to another in a circular orbit around the Earth to validate its effectiveness. &#169; 2011 IFAC.</description.abstract>
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<subject>Delay independent</subject>
<subject>Delay-dependent</subject>
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Author Affiliations
  1. University of Virginia
  2. The University of Hong Kong
  3. Harbin Institute of Technology