재사용 발사체의 3-루프 기반 비선형 자세 제어기 설계Nonlinear Attitude Controller for Reusable Launch Vehicles via Three-loop Topology

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Publisher
한국항공우주학회
Issue Date
2020-07-08
Language
Korean
Citation

한국항공우주학회 2020년도 춘계학술대회

URI
http://hdl.handle.net/10203/278274
Appears in Collection
AE-Conference Papers(학술회의논문)
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