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비행제어법칙 감항인증 기준 설정 및 입증 연구

A Study for the Airworthiness Certification Criteria and Compliance Related to the Flight Control Law

  • Koh, Gi Ok (Korea Aerospace Industries) ;
  • Ko, Joon Soo (Korea Aerospace University, School of Aeronautical & Mechanical Engineering) ;
  • An, Young Gab (Defense Agency for Technology and Quality)
  • 투고 : 2012.12.28
  • 심사 : 2013.06.25
  • 발행 : 2013.07.01

초록

군용항공기 산업의 비약적인 발전으로 정부의 군용항공기 감항인증은 점차적으로 중요한 역할을 차지하고 있다. 감항인증은 모든 항공기가 전 수명주기 동안 운용범위 내에서 비행안전에 적합하도록 항공기 개발에 필수적으로 요구되는 절차이다. 감항인증의 도입은 단일 수요자의 요구도에 부합되게 개발 해왔던 기존의 개발 사업특성에서 다수의 수요자의 공통의 요구도를 맞춘 개발 패러다임의 변화로 이끌어 가고 있다. 본 논문에서는 전투기급 항공기의 비행제어법칙의 감항인증 기준 설정에 대한 상세 연구와 감항인증 기술기준에 대한 입증 분석을 결과로 제시하였다.

The Airworthiness Certification from the government has an increasingly important role due to the dramatic growth of military aircraft development industry. It is a mandatory process of qualifying the flight safety within the aircraft's operational boundaries throughout its life cycle. The introduction of airworthiness certification has resulted in development paradigm shift from one requirement for one consumer need to the common requirement for many needs. This research paper provide the refinement of airworthiness certification criteria related to the flight control law and the verification methods which comply with its criteria.

키워드

참고문헌

  1. DAPA, "DAPA Notice 2011-1 Military Aircraft Airworthiness Certification Criteria", 2011.12.7
  2. Secretary of Air Force, 2019 7.11, 'Air Force Directorate 62-6"
  3. Kwon Wook Hyun, 1999.1.10. "Control System Engineering, Part 7", Chung Moon Gak
  4. MIL_DTL_9490E,"Flight Control systems - Design, Installation and Test of Piloted Aircraft", 2008.4.2
  5. DoD Joint Specification Guide, "JSSG-2008 Vehicle Control and Management System (VCMS)",1998. 10. 30
  6. DoD Joint Specification Guide, "JSSG-2001 Air Vehicle", 2004.4.30
  7. KAI, "FA-50 Control Law Analysis Report", 2012.3.27
  8. G.E.Cooper, R.P.Harper,Jr, Apr,1969, " The use of Pilot Rating in the Evaluation of Aircraft Handling Qualities", NASA TN D-5153
  9. KAI, "FA-50 Test Information Sheet for Flight Controls & Handling Quality Tests", 2010.9.30
  10. KAI, "System Test Report for the Flight control Computer Operational Flight Program FF53F for the Republic of Korea", 2012.5.17

피인용 문헌

  1. Airworthiness Case Study for the Tactical UAV's Flight Control System vol.17, pp.4, 2014, https://doi.org/10.9766/KIMST.2014.17.4.430