Data-Enabled Predictive Control for Flexible SpacecraftSource: Journal of Dynamic Systems, Measurement, and Control:;2026:;volume( 148 ):;issue:006::page 3311Author:Wang, Huanqing
,
Zhang, Kaixiang
,
Vahidi-Moghaddam, Amin
,
An, Haowei
,
Li, Nan
,
Huang, Daning
,
Li, Zhaojian
DOI: 10.1115/1.4071867Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Abstract. 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.
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| contributor author | Wang, Huanqing | |
| contributor author | Zhang, Kaixiang | |
| contributor author | Vahidi-Moghaddam, Amin | |
| contributor author | An, Haowei | |
| contributor author | Li, Nan | |
| contributor author | Huang, Daning | |
| contributor author | Li, Zhaojian | |
| date accessioned | 2026-08-23T07:15:53Z | |
| date available | 2026-08-23T07:15:53Z | |
| date copyright | 2026/11/01 | |
| date issued | 2026 | |
| identifier issn | 0022-0434 | |
| identifier other | ds-25-1115.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314858 | |
| description abstract | Abstract. 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. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Data-Enabled Predictive Control for Flexible Spacecraft | |
| type | Journal Paper | |
| journal volume | 148 | |
| journal issue | 6 | |
| journal title | Journal of Dynamic Systems, Measurement, and Control | |
| identifier doi | 10.1115/1.4071867 | |
| journal fristpage | 3311 | |
| journal lastpage | 3320 | |
| page | 10 | |
| tree | Journal of Dynamic Systems, Measurement, and Control:;2026:;volume( 148 ):;issue:006 | |
| contenttype | Fulltext |