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Decentralized Sliding Mode Control for a Spacecraft Flexible Appendage Based on Finite Element Method

✍ Scribed by Yong-an HUANG; Zi-chen DENG

Book ID: 114335449
Publisher: Elsevier Science
Year: 2005
Tongue: English
Weight: 357 KB
Volume: 18
Category: Article
ISSN: 1000-9361
DOI: 10.1016/s1000-9361(11)60303-8

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