Browse
S-Space
College of Engineering/Engineering Practice School (공과대학/대학원)
Dept. of Mechanical Aerospace Engineering (기계항공공학부)
Theses (Ph.D. / Sc.D._기계항공공학부)
위성발사체의 궤적최적화와 관성유도 알고리듬 설계에 관한 연구 : A Study on the trajectory optimization and inertial guidance algorithm design for satellite launch vehicles
- 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
- Files in This Item: There are no files associated with this item.
Items in S-Space are protected by copyright, with all rights reserved, unless otherwise indicated.