Relative angles-only navigation for satellite relative motion = 위성간 각도정보를 활용한 인공위성의 상대운동 항법 연구

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In this thesis, relative angles-only navigation for satellite relative motion is studied. Since angles-only measurement has no range information, appropriate transfer trajectory of the chaser satellite should be designed taking into the observability. For the observability criteria, the Fisher information matrix is used. In addition, the fuel consumption is also considered for the trajectory design. By using the criteria, the trajectory is designed based on the basic transfer trajectories. For verification, numerical simulations are presented using the Extended kalman filter.
Advisors
Bang, Hyo-Choongresearcher방효충researcher
Description
한국과학기술원 : 항공우주공학전공,
Publisher
한국과학기술원
Issue Date
2011
Identifier
467980/325007  / 020093571
Language
eng
Description

학위논문(석사) - 한국과학기술원 : 항공우주공학전공, 2011.2, [ iv, 43 p. ]

Keywords

Fisher information matrix; Trajectory design; Satellite relative motion; Angles-only navigation; Glideslope approach; 글라이드슬로프 접근법; 피셔 정보 행렬; 궤적 설계; 인공위성 상대운동; 베어링 항법

URI
http://hdl.handle.net/10203/26484
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=467980&flag=dissertation
Appears in Collection
AE-Theses_Master(석사논문)
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