Sliding mode control for low-thrust Earth-orbiting spacecraft formation maneuvering | |
Liu Hui ; Li Junfeng ; Hexi Baoyin | |
2010-05-10 ; 2010-05-10 ; OCT | |
关键词 | spacecraft formation flying sliding mode control entire-formation maneuvering MULTIPLE SPACECRAFT SYSTEMS Engineering, Aerospace |
中文摘要 | This paper considers the control of entire-formation maneuvering in low-thrust Earth-orbiting spacecraft formation flying (SFF). A coordinated control scheme based on the leader-follower approach is developed to achieve formation maneuvers while keeping the internal formation intact. To implement the control scheme, a low-level sliding mode control (SMC) based on nonlinear dynamics is provided. Using a Lyapunov-based control design and stability analysis technique, we prove that the closed-loop system is globally asymptotically stable. Numerical simulations show the advantage of the controller for fuel cost reductions, tracking accuracy, and effectiveness in ensuring entire-formation maneuvering. An exact nonlinear model with modeled disturbances (J(2) disturbance and bounded uncertainties) is used for dynamic simulation. (c) 2006 Elsevier Masson SAS. All rights reserved. |
语种 | 英语 ; 英语 |
出版者 | ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER ; PARIS ; 23 RUE LINOIS, 75724 PARIS, FRANCE |
内容类型 | 期刊论文 |
源URL | [http://hdl.handle.net/123456789/22541] |
专题 | 清华大学 |
推荐引用方式 GB/T 7714 | Liu Hui,Li Junfeng,Hexi Baoyin. Sliding mode control for low-thrust Earth-orbiting spacecraft formation maneuvering[J],2010, 2010, OCT. |
APA | Liu Hui,Li Junfeng,&Hexi Baoyin.(2010).Sliding mode control for low-thrust Earth-orbiting spacecraft formation maneuvering.. |
MLA | Liu Hui,et al."Sliding mode control for low-thrust Earth-orbiting spacecraft formation maneuvering".(2010). |
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