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- Publisher Website: 10.1109/TCST.2016.2632529
- Scopus: eid_2-s2.0-85009834007
- WOS: WOS:000413143800024
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Article: Global Stabilization of Linearized Spacecraft Rendezvous System by Saturated Linear Feedback
Title | Global Stabilization of Linearized Spacecraft Rendezvous System by Saturated Linear Feedback |
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Authors | |
Keywords | Actuator saturation Global stabilization Linear feedback Spacecraft rendezvous |
Issue Date | 2017 |
Publisher | IEEE. The Journal's web site is located at http://ieeexplore.ieee.org/xpl/RecentIssue.jsp?punumber=87 |
Citation | IEEE Transactions on Control Systems Technology, 2017, v. 25 n. 6, p. 2185-2193 How to Cite? |
Abstract | The problem of global stabilization of the circular orbit spacecraft rendezvous system subject to actuator saturation is studied in this brief. Based on the linearized Clohessy-Wiltshire equations, a class of saturated linear state feedback controllers is designed by utilizing Lyapunov functions that are frequently used in the absolute stability theory. The global stability of the closed-loop system with the proposed saturated linear feedback is proved by providing explicit conditions on the parameters in the feedback gains. Optimal linear feedback gains are also discussed. The most significant advantages of the proposed controllers are that the controllers are linear and the global stability of the resulting closed-loop system can be guaranteed. Numerical simulations show the effectiveness of the proposed approaches. |
Persistent Identifier | http://hdl.handle.net/10722/262346 |
ISSN | 2023 Impact Factor: 4.9 2023 SCImago Journal Rankings: 2.193 |
ISI Accession Number ID |
DC Field | Value | Language |
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dc.contributor.author | Zhou, B | - |
dc.contributor.author | Lam, J | - |
dc.date.accessioned | 2018-09-28T04:57:45Z | - |
dc.date.available | 2018-09-28T04:57:45Z | - |
dc.date.issued | 2017 | - |
dc.identifier.citation | IEEE Transactions on Control Systems Technology, 2017, v. 25 n. 6, p. 2185-2193 | - |
dc.identifier.issn | 1063-6536 | - |
dc.identifier.uri | http://hdl.handle.net/10722/262346 | - |
dc.description.abstract | The problem of global stabilization of the circular orbit spacecraft rendezvous system subject to actuator saturation is studied in this brief. Based on the linearized Clohessy-Wiltshire equations, a class of saturated linear state feedback controllers is designed by utilizing Lyapunov functions that are frequently used in the absolute stability theory. The global stability of the closed-loop system with the proposed saturated linear feedback is proved by providing explicit conditions on the parameters in the feedback gains. Optimal linear feedback gains are also discussed. The most significant advantages of the proposed controllers are that the controllers are linear and the global stability of the resulting closed-loop system can be guaranteed. Numerical simulations show the effectiveness of the proposed approaches. | - |
dc.language | eng | - |
dc.publisher | IEEE. The Journal's web site is located at http://ieeexplore.ieee.org/xpl/RecentIssue.jsp?punumber=87 | - |
dc.relation.ispartof | IEEE Transactions on Control Systems Technology | - |
dc.rights | IEEE Transactions on Control Systems Technology. Copyright © IEEE. | - |
dc.subject | Actuator saturation | - |
dc.subject | Global stabilization | - |
dc.subject | Linear feedback | - |
dc.subject | Spacecraft rendezvous | - |
dc.title | Global Stabilization of Linearized Spacecraft Rendezvous System by Saturated Linear Feedback | - |
dc.type | Article | - |
dc.identifier.email | Lam, J: jlam@hku.hk | - |
dc.identifier.authority | Lam, J=rp00133 | - |
dc.description.nature | link_to_subscribed_fulltext | - |
dc.identifier.doi | 10.1109/TCST.2016.2632529 | - |
dc.identifier.scopus | eid_2-s2.0-85009834007 | - |
dc.identifier.hkuros | 291927 | - |
dc.identifier.volume | 25 | - |
dc.identifier.issue | 6 | - |
dc.identifier.spage | 2185 | - |
dc.identifier.epage | 2193 | - |
dc.identifier.isi | WOS:000413143800024 | - |
dc.publisher.place | United States | - |
dc.identifier.issnl | 1063-6536 | - |