Decentralized Sliding Mode Control for a Spacecraft Flexible Appendage Based on Finite Element Method
نویسندگان
چکیده
منابع مشابه
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ژورنال
عنوان ژورنال: Chinese Journal of Aeronautics
سال: 2005
ISSN: 1000-9361
DOI: 10.1016/s1000-9361(11)60303-8