Please use this identifier to cite or link to this item:
Title: Non-model-based robust controller design for flexible spacecraft
Authors: Ge, S.S. 
Lee, T.H. 
Hong, F. 
Goh, C.H.
Issue Date: 2000
Citation: Ge, S.S.,Lee, T.H.,Hong, F.,Goh, C.H. (2000). Non-model-based robust controller design for flexible spacecraft. Proceedings of the IEEE Conference on Decision and Control 4 : 3785-3790. ScholarBank@NUS Repository.
Abstract: This paper presents a class of non-model-based position controllers for a kind of flexible spacecraft. A very basic system energy relationship of the flexible spacecraft is involved in the controller design and stability analysis instead of system dynamics themselves. With the controllers, one can achieve not only the closed-loop stability of the original distributed-parameter system, but also the asymptotic stability of the truncated system, which is obtained through representing the deflection of the appendage by an arbitrary finite number of flexible modes. Simulation results carried out on a kind of spacecraft with one flexible appendage justify the effectiveness of the proposed controller.
Source Title: Proceedings of the IEEE Conference on Decision and Control
ISSN: 01912216
Appears in Collections:Staff Publications

Show full item record
Files in This Item:
There are no files associated with this item.

Page view(s)

checked on Jun 23, 2022

Google ScholarTM


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.