Enhanced attitude tracking control of spacecraft via inner and outer loop sliding mode design.
The significance of spacecraft in modern aerospace and technology is indisputable, with attitude control systems (ACS) playing a vital role in ensuring mission accuracy and safety. This study presents a dual-loop sliding mode variable structure control approach for spacecraft attitude regulation, le...
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| Format: | Article |
| Language: | English |
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Public Library of Science (PLoS)
2025-01-01
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| Series: | PLoS ONE |
| Online Access: | https://doi.org/10.1371/journal.pone.0328622 |
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| author | Xinxiang Fang Ming Wen |
| author_facet | Xinxiang Fang Ming Wen |
| author_sort | Xinxiang Fang |
| collection | DOAJ |
| description | The significance of spacecraft in modern aerospace and technology is indisputable, with attitude control systems (ACS) playing a vital role in ensuring mission accuracy and safety. This study presents a dual-loop sliding mode variable structure control approach for spacecraft attitude regulation, leveraging integral sliding mode control (SMC) to design robust switching functions. The outer loop generates the angular velocity command [Formula: see text] by tracking the desired attitude angle [Formula: see text], while the inner loop ensures accurate torque control based on this command. The control architecture comprises an inner velocity loop and an outer position loop, with the inner loop deliberately designed to converge faster, ensuring overall system stability. Numerical simulations validate the proposed strategy's effectiveness and highlight its potential for real-world aerospace applications. |
| format | Article |
| id | doaj-art-029526943fcd441dbd83ffbf0c58014e |
| institution | DOAJ |
| issn | 1932-6203 |
| language | English |
| publishDate | 2025-01-01 |
| publisher | Public Library of Science (PLoS) |
| record_format | Article |
| series | PLoS ONE |
| spelling | doaj-art-029526943fcd441dbd83ffbf0c58014e2025-08-20T03:12:34ZengPublic Library of Science (PLoS)PLoS ONE1932-62032025-01-01207e032862210.1371/journal.pone.0328622Enhanced attitude tracking control of spacecraft via inner and outer loop sliding mode design.Xinxiang FangMing WenThe significance of spacecraft in modern aerospace and technology is indisputable, with attitude control systems (ACS) playing a vital role in ensuring mission accuracy and safety. This study presents a dual-loop sliding mode variable structure control approach for spacecraft attitude regulation, leveraging integral sliding mode control (SMC) to design robust switching functions. The outer loop generates the angular velocity command [Formula: see text] by tracking the desired attitude angle [Formula: see text], while the inner loop ensures accurate torque control based on this command. The control architecture comprises an inner velocity loop and an outer position loop, with the inner loop deliberately designed to converge faster, ensuring overall system stability. Numerical simulations validate the proposed strategy's effectiveness and highlight its potential for real-world aerospace applications.https://doi.org/10.1371/journal.pone.0328622 |
| spellingShingle | Xinxiang Fang Ming Wen Enhanced attitude tracking control of spacecraft via inner and outer loop sliding mode design. PLoS ONE |
| title | Enhanced attitude tracking control of spacecraft via inner and outer loop sliding mode design. |
| title_full | Enhanced attitude tracking control of spacecraft via inner and outer loop sliding mode design. |
| title_fullStr | Enhanced attitude tracking control of spacecraft via inner and outer loop sliding mode design. |
| title_full_unstemmed | Enhanced attitude tracking control of spacecraft via inner and outer loop sliding mode design. |
| title_short | Enhanced attitude tracking control of spacecraft via inner and outer loop sliding mode design. |
| title_sort | enhanced attitude tracking control of spacecraft via inner and outer loop sliding mode design |
| url | https://doi.org/10.1371/journal.pone.0328622 |
| work_keys_str_mv | AT xinxiangfang enhancedattitudetrackingcontrolofspacecraftviainnerandouterloopslidingmodedesign AT mingwen enhancedattitudetrackingcontrolofspacecraftviainnerandouterloopslidingmodedesign |