지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술대회자료
- 저자정보
- 발행연도
- 2014.4
- 수록면
- 424 - 428 (5page)
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초록· 키워드
오류제보하기
This paper describes a framework development using system engineering concept for various space launch vehicles to assist engineers during mission design process. This design framework integrates many different functions and capabilities: data mining for estimation and optimization of initial values, data analysis of each module, sequential optimization of each module, entire optimization of all modules, and geometric 3D modeling of final configuration of target space launch vehicle. Furthermore, the tool was designed to accept and save input values from users, and run the optimization after being prepared. Alternatively, the user can load and run system-default values to know how exactly the framework works. The design framework was developed using a high-level technical computing language and interactive environment of MATLAB and 3D modeling using CATIA v5. With this space launch framework, the mission design for the rocket system targeted on the 700 x 700 km circular orbit has been successfully performed to demonstrate the efficiency of the framework.
목차
ABSTRACT
1. Introduction
2. Detailed Description of The Framework
3. Description of Sub-modules
4. Design Completion
5. Conclusion and Future Works
References
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UCI(KEPA) : I410-ECN-0101-2016-558-000998492