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위성발사체의 궤적최적화와 관성유도 알고리듬 설계에 관한 연구 : A Study on the trajectory optimization and inertial guidance algorithm design for satellite launch vehicles
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- Authors
- Advisor
- 김유단
- Issue Date
- 2001
- Publisher
- 서울대학교 대학원
- Keywords
- atellite launch vehicle ; 위성발사체 ; trajectory optimization ; 궤적최적화 ; time finite element method ; 시간유한요소법 ; direct collocation ; 준상태변수추정 ; costate estimation ; 관성유도
- Description
- 학위논문(박사)--서울대학교 대학원 :항공우주공학과,2001.
- Language
- Korean
- URI
- http://dcollection.snu.ac.kr:80/jsp/common/DcLoOrgPer.jsp?sItemId=000000066357
https://hdl.handle.net/10371/31721
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