Generalized missile guidance law for impact angle control = 일반화된 충돌각 제어 유도법칙 연구

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Advisors
Tahk, Min-Jearesearcher탁민제
Description
한국과학기술원 : 항공우주공학전공,
Publisher
한국과학기술원
Issue Date
2012
Identifier
487163/325007  / 020085308
Language
eng
Description

학위논문(박사) - 한국과학기술원 : 항공우주공학전공, 2012.2, [ vii, 128 p. ]

Keywords

impact angle control; guidance law; optimality; analytic solution; 유도법칙; 충돌각 제어; 최적성; 해석해; 시스템 지연; system lag

URI
http://hdl.handle.net/10203/179632
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=487163&flag=dissertation
Appears in Collection
AE-Theses_Ph.D.(박사논문)
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