Attitude Stabilization Control for Underactuated Spacecraft: A Predefined-Time Method Article Swipe
Yuzhu Bai
,
Yuyao Wu
,
Jie Wen
·
YOU?
·
· 2025
· Open Access
·
· DOI: https://doi.org/10.34133/space.0272
YOU?
·
· 2025
· Open Access
·
· DOI: https://doi.org/10.34133/space.0272
The attitude controller design for the underactuated rigid spacecraft is addressed by considering that there are only 2 reaction wheels in the spacecraft. Most of the existing attitude control methods for underactuated spacecraft suffer from long system state convergence times and large overshoots. To improve the rapidity and stability of the attitude control system, in this paper, the predefined-time control technique is investigated for solving the attitude stabilization control issue for the underactuated spacecraft for the first time. By combining the sliding control method, a kind of predefined-time attitude stabilization control scheme is developed for the underactuated spacecraft. It is shown that the attitude variables and the angular velocity of the underactuated spacecraft are convergent into 2 non-empty sets within a predefined time by theoretical analysis. The simulation results illustrate the predefined-time convergence of the presented control scheme. In addition, the advantages of the proposed control strategy in this paper are demonstrated by comparing it with some existing control methods.
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- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.34133/space.0272
- OA Status
- diamond
- Cited By
- 1
- References
- 25
- Related Works
- 10
- OpenAlex ID
- https://openalex.org/W4409448192
All OpenAlex metadata
Raw OpenAlex JSON
- OpenAlex ID
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https://openalex.org/W4409448192Canonical identifier for this work in OpenAlex
- DOI
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https://doi.org/10.34133/space.0272Digital Object Identifier
- Title
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Attitude Stabilization Control for Underactuated Spacecraft: A Predefined-Time MethodWork title
- Type
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articleOpenAlex work type
- Language
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enPrimary language
- Publication year
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2025Year of publication
- Publication date
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2025-01-01Full publication date if available
- Authors
-
Yuzhu Bai, Yuyao Wu, Jie WenList of authors in order
- Landing page
-
https://doi.org/10.34133/space.0272Publisher landing page
- Open access
-
YesWhether a free full text is available
- OA status
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diamondOpen access status per OpenAlex
- OA URL
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https://doi.org/10.34133/space.0272Direct OA link when available
- Concepts
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Underactuation, Control theory (sociology), Spacecraft, Control (management), Computer science, Attitude control, Control engineering, Engineering, Aerospace engineering, Artificial intelligenceTop concepts (fields/topics) attached by OpenAlex
- Cited by
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1Total citation count in OpenAlex
- Citations by year (recent)
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2025: 1Per-year citation counts (last 5 years)
- References (count)
-
25Number of works referenced by this work
- Related works (count)
-
10Other works algorithmically related by OpenAlex
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