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Finite-Time Contractive Control of Spacecraft Rendezvous System

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Název: Finite-Time Contractive Control of Spacecraft Rendezvous System
Autoři: Jing Sheng, Yunhai Geng, Min Li, Baolong Zhu
Zdroj: Mathematics, Vol 11, Iss 8, p 1871 (2023)
Informace o vydavateli: MDPI AG
Rok vydání: 2023
Sbírka: Directory of Open Access Journals: DOAJ Articles
Témata: finite-time contractive stability, state feedback control, spacecraft rendezvous system, cone complementary linearization, C-W equations, Mathematics, QA1-939
Popis: In this paper we investigate the problem of a finite-time contractive control method for a spacecraft rendezvous control system. The dynamic model of relative motion is formulated by the C-W equations. To improve the convergent performance of the spacecraft rendezvous control system, a finite-time contractive control law is introduced. Lyapunov’s direct method is employed to obtain the existence condition of the desired controllers. The controller parameter can be obtained with the help of the cone complementary linearization algorithm. A numerical example verifies the effectiveness of the obtained theoretical results.
Druh dokumentu: article in journal/newspaper
Jazyk: English
Relation: https://www.mdpi.com/2227-7390/11/8/1871; https://doaj.org/toc/2227-7390; https://doaj.org/article/71bb0407074345ffb37bd301c66396c3
DOI: 10.3390/math11081871
Dostupnost: https://doi.org/10.3390/math11081871
https://doaj.org/article/71bb0407074345ffb37bd301c66396c3
Přístupové číslo: edsbas.F4396EB6
Databáze: BASE
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  Data: Finite-Time Contractive Control of Spacecraft Rendezvous System
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  Data: <searchLink fieldCode="AR" term="%22Jing+Sheng%22">Jing Sheng</searchLink><br /><searchLink fieldCode="AR" term="%22Yunhai+Geng%22">Yunhai Geng</searchLink><br /><searchLink fieldCode="AR" term="%22Min+Li%22">Min Li</searchLink><br /><searchLink fieldCode="AR" term="%22Baolong+Zhu%22">Baolong Zhu</searchLink>
– Name: TitleSource
  Label: Source
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  Data: Mathematics, Vol 11, Iss 8, p 1871 (2023)
– Name: Publisher
  Label: Publisher Information
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  Data: MDPI AG
– Name: DatePubCY
  Label: Publication Year
  Group: Date
  Data: 2023
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  Data: Directory of Open Access Journals: DOAJ Articles
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  Data: <searchLink fieldCode="DE" term="%22finite-time+contractive+stability%22">finite-time contractive stability</searchLink><br /><searchLink fieldCode="DE" term="%22state+feedback+control%22">state feedback control</searchLink><br /><searchLink fieldCode="DE" term="%22spacecraft+rendezvous+system%22">spacecraft rendezvous system</searchLink><br /><searchLink fieldCode="DE" term="%22cone+complementary+linearization%22">cone complementary linearization</searchLink><br /><searchLink fieldCode="DE" term="%22C-W+equations%22">C-W equations</searchLink><br /><searchLink fieldCode="DE" term="%22Mathematics%22">Mathematics</searchLink><br /><searchLink fieldCode="DE" term="%22QA1-939%22">QA1-939</searchLink>
– Name: Abstract
  Label: Description
  Group: Ab
  Data: In this paper we investigate the problem of a finite-time contractive control method for a spacecraft rendezvous control system. The dynamic model of relative motion is formulated by the C-W equations. To improve the convergent performance of the spacecraft rendezvous control system, a finite-time contractive control law is introduced. Lyapunov’s direct method is employed to obtain the existence condition of the desired controllers. The controller parameter can be obtained with the help of the cone complementary linearization algorithm. A numerical example verifies the effectiveness of the obtained theoretical results.
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  Data: English
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  Data: https://www.mdpi.com/2227-7390/11/8/1871; https://doaj.org/toc/2227-7390; https://doaj.org/article/71bb0407074345ffb37bd301c66396c3
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  Data: 10.3390/math11081871
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  Data: https://doi.org/10.3390/math11081871<br />https://doaj.org/article/71bb0407074345ffb37bd301c66396c3
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      – Text: English
    Subjects:
      – SubjectFull: finite-time contractive stability
        Type: general
      – SubjectFull: state feedback control
        Type: general
      – SubjectFull: spacecraft rendezvous system
        Type: general
      – SubjectFull: cone complementary linearization
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      – SubjectFull: C-W equations
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