Discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation

This paper studies the discrete gain scheduling control design problem of elliptical orbit spacecraft rendezvous system with actuator saturation. Due to the presence of actuator saturation, the dynamic performance of the spacecraft rendezvous system degrades significantly. In order to improve the dy...

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Main Authors: Gao, X., He, D., Teo, Kok Lay, Wang, J., Yang, H.
Format: Journal Article
Published: 2023
Online Access:http://purl.org/au-research/grants/arc/DP190103361
http://hdl.handle.net/20.500.11937/94745
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author Gao, X.
He, D.
Teo, Kok Lay
Wang, J.
Yang, H.
author_facet Gao, X.
He, D.
Teo, Kok Lay
Wang, J.
Yang, H.
author_sort Gao, X.
building Curtin Institutional Repository
collection Online Access
description This paper studies the discrete gain scheduling control design problem of elliptical orbit spacecraft rendezvous system with actuator saturation. Due to the presence of actuator saturation, the dynamic performance of the spacecraft rendezvous system degrades significantly. In order to improve the dynamic performance of the system, a discrete gain scheduling control approach is adopted to construct a group of time-invariant ellipsoidal invariant sets, which can be used to determine the switching points of the discrete gain scheduling control. By choosing some discrete parameter values, the discrete gain scheduling control is obtained from a solution of a periodic Riccati matrix differential equation. Under the control obtained, the dynamic performance of the system is much improved while accomplishing successfully the rendezvous mission of the spacecraft. Finally, a practical example is provided to show the effectiveness of the proposed control design approach.
first_indexed 2025-11-14T11:42:47Z
format Journal Article
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institution Curtin University Malaysia
institution_category Local University
last_indexed 2025-11-14T11:42:47Z
publishDate 2023
recordtype eprints
repository_type Digital Repository
spelling curtin-20.500.11937-947452024-04-10T09:07:17Z Discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation Gao, X. He, D. Teo, Kok Lay Wang, J. Yang, H. This paper studies the discrete gain scheduling control design problem of elliptical orbit spacecraft rendezvous system with actuator saturation. Due to the presence of actuator saturation, the dynamic performance of the spacecraft rendezvous system degrades significantly. In order to improve the dynamic performance of the system, a discrete gain scheduling control approach is adopted to construct a group of time-invariant ellipsoidal invariant sets, which can be used to determine the switching points of the discrete gain scheduling control. By choosing some discrete parameter values, the discrete gain scheduling control is obtained from a solution of a periodic Riccati matrix differential equation. Under the control obtained, the dynamic performance of the system is much improved while accomplishing successfully the rendezvous mission of the spacecraft. Finally, a practical example is provided to show the effectiveness of the proposed control design approach. 2023 Journal Article http://hdl.handle.net/20.500.11937/94745 10.1002/rnc.6509 http://purl.org/au-research/grants/arc/DP190103361 fulltext
spellingShingle Gao, X.
He, D.
Teo, Kok Lay
Wang, J.
Yang, H.
Discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation
title Discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation
title_full Discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation
title_fullStr Discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation
title_full_unstemmed Discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation
title_short Discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation
title_sort discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation
url http://purl.org/au-research/grants/arc/DP190103361
http://hdl.handle.net/20.500.11937/94745