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dc.contributor.authorWang, Huanqing
dc.contributor.authorZhang, Kaixiang
dc.contributor.authorVahidi-Moghaddam, Amin
dc.contributor.authorAn, Haowei
dc.contributor.authorLi, Nan
dc.contributor.authorHuang, Daning
dc.contributor.authorLi, Zhaojian
dc.date.accessioned2026-08-23T07:15:53Z
dc.date.available2026-08-23T07:15:53Z
dc.date.copyright2026/11/01
dc.date.issued2026
dc.identifier.issn0022-0434
dc.identifier.otherds-25-1115.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314858
dc.description.abstractAbstract. Spacecraft are vital to space exploration and are often equipped with lightweight, flexible appendages to meet strict weight constraints. These appendages pose significant challenges for modeling and control due to their inherent nonlinearity. Data-driven control methods have gained traction to address such challenges. This paper introduces, to the best of the authors' knowledge, the first application of the data-enabled predictive control (DeePC) framework to boundary control for flexible spacecraft. Leveraging the fundamental lemma, DeePC constructs a nonparametric model by utilizing recorded past trajectories, eliminating the need for explicit model development. The developed method also incorporates dimension reduction techniques to enhance computational efficiency. Through numerical simulations, the proposed method is compared with a model-based Lyapunov boundary control approach, demonstrating robust performance under uncertainty, noise, and disturbances.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleData-Enabled Predictive Control for Flexible Spacecraft
dc.typeJournal Paper
dc.journal.volume148
dc.journal.issue6
dc.journal.titleJournal of Dynamic Systems, Measurement, and Control
dc.identifier.doi10.1115/1.4071867
dc.journal.fristpage3311
dc.journal.lastpage3320
dc.page10
dc.treeJournal of Dynamic Systems, Measurement, and Control:;2026:;volume( 148 ):;issue:006
dc.contenttypeFulltext


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