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
- 학술저널
- 저자정보
- 저널정보
- 한국항공우주학회 International Journal of Aeronautical and Space Sciences International Journal of Aeronautical and Space Sciences Volume.13 Number.4
- 발행연도
- 2012.12
- 수록면
- 435 - 445 (11page)
이용수
초록· 키워드
오류제보하기
In this paper, a design process is established by integrating aviation safety requirements for the development of general aviation aircraft. An Airworthiness?Design Integration System, which integrates certification requirements with the entire design/analysis process, is developed and presented. For the proposed system, KAS 23/FAR 23/AC 23/CS 23 certification regulations are analyzed to determine design constraints and system compliance checks and to construct an ER&G (Engineering Requirement and Guide) and a Design-Certification Related Table (DCRT). Furthermore, through building a DB (Data Base), the management of design and certification related resources for developing a FAR 23 class aircraft are made. Certification tools and resources are also efficiently managed by the DB. The connection between the certification requirements and the detailed design process is proposed in this system. Tracking of this proposed method is validated by configuring a USE CASE and a system. The Airworthiness?Design Integration system will be constructed based on the system’s design plan, certification system, and usage scenarios.
목차
Abstract
1. Introduction
2. Aircraft Airworthiness-Design Integrated System
3. Case Study of Aircraft Design Program
4. Conclusion
Acknowledgement
References
참고문헌 (17)
참고문헌 신청
Cho, G. H. / 2008 / Small Aircraft Certification Process during Design and Development Stage / Conference of Korea Society for Aeronautical and Space Science, Pyeongchang, Korea
Levine, W. S. / 1999 / CONDUIT-Control Designer’s Unified Interface / Computer Aided Control System Design, 1999. Proceedings of the 1999 IEEE International Symposium, Hawaii, UAS
Colbourne, J. / 1999 / The Development of the CONDUIT Advanced Control System Design and Evaluation Interface with a Case Study Application to an Advanced Fly by Wire Helicopter Design / NASA/TM-1999-208763, AFDD/TR-99-A-005
Calin Gologan / PC-Aero
Eric, L. / 2010 / A framework for testing DBMS features / The VLDB Journal 19(2):203~230
Levine, W. S. / 1999 / CONDUIT-Control Designer’s Unified Interface / Computer Aided Control System Design, 1999. Proceedings of the 1999 IEEE International Symposium, Hawaii, UAS
Colbourne, J. / 1999 / The Development of the CONDUIT Advanced Control System Design and Evaluation Interface with a Case Study Application to an Advanced Fly by Wire Helicopter Design / NASA/TM-1999-208763, AFDD/TR-99-A-005
Calin Gologan / PC-Aero
Eric, L. / 2010 / A framework for testing DBMS features / The VLDB Journal 19(2):203~230
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