OUTPUT FEEDBACK SLEWING CONTROL OF FLEWIBLE SPACECRAFT BY LYAPUNOV STABILITY THEORY - koreascholar

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OUTPUT FEEDBACK SLEWING CONTROL OF FLEWIBLE SPACECRAFT BY LYAPUNOV STABILITY THEORY KCI 등재 SCOPUS

Kim, Dae-Sik, Kim, Chun-Hwey, Bang, Hyo-Choong

언어ENG
URLhttps://db.koreascholar.com/Article/Detail/267015

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Journal of Astronomy and Space Sciences

제14권 2호 (1997.12)
pp.367-374

한국우주과학회 (The Korean Space Science Society)

저자

Kim, Dae-Sik(Department of Astronomy & Space Science, Chungbuk National University)
Kim, Chun-Hwey( Department of Astronomy & Space Science, Chungbuk National University) | Kim, Chun-Hwey
Bang, Hyo-Choong( KOREASAT Group, Korea Aerospace Research Institute) | Bang, Hyo-Choong

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