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contributor authorWang, Huanqing
contributor authorZhang, Kaixiang
contributor authorVahidi-Moghaddam, Amin
contributor authorAn, Haowei
contributor authorLi, Nan
contributor authorHuang, Daning
contributor authorLi, Zhaojian
date accessioned2026-08-23T07:15:53Z
date available2026-08-23T07:15:53Z
date copyright2026/11/01
date issued2026
identifier issn0022-0434
identifier otherds-25-1115.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314858
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.
publisherThe American Society of Mechanical Engineers (ASME)
titleData-Enabled Predictive Control for Flexible Spacecraft
typeJournal Paper
journal volume148
journal issue6
journal titleJournal of Dynamic Systems, Measurement, and Control
identifier doi10.1115/1.4071867
journal fristpage3311
journal lastpage3320
page10
treeJournal of Dynamic Systems, Measurement, and Control:;2026:;volume( 148 ):;issue:006
contenttypeFulltext


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