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College of Engineering(공과대학)School of Mechanical and Aerospace Engineering(기계항공공학부)Dept. of Aerospace Engineering(항공우주공학과)AE-Journal Papers(저널논문)

OUTPUT FEEDBACK SLEWING CONTROL OF FLEXIBLE SPACECRAFT BY LYAPUNOV STABILITY THEORY

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김대식 / 김천휘 / 방효충researcher
Publisher
한국우주과학회
Issue Date
1997-12
Language
Korean
Citation

JOURNAL OF ASTRONOMY AND SPACE SCIENCES, v.14, no.2, pp.367 - 374

ISSN
1598-5601
URI
http://hdl.handle.net/10203/69246
Appears in Collection
AE-Journal Papers(저널논문)
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