쿼터니언을 이용한 인공위성 자세제어기법 연구Satellite attitude control using quaternion parameters

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Advisors
탁민제researcherTahk, Min-Jaeresearcher
Description
한국과학기술원 : 항공우주공학과,
Publisher
한국과학기술원
Issue Date
1996
Identifier
105568/325007 / 000943368
Language
kor
Description

학위논문(석사) - 한국과학기술원 : 항공우주공학과, 1996.2, [ vii, 74 p. ]

Keywords

모멘텀 덤프; 반동휠; 고유축 회전; 쿼터니언; 지구자기모델; IGRF; Momentum Dump; Reaction Wheel; Eigenaxis Rotation; Quaternion

URI
http://hdl.handle.net/10203/26774
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=105568&flag=dissertation
Appears in Collection
AE-Theses_Master(석사논문)
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