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Relex를 이용한 항공기 시스템 안전성 평가 절차 사례분석

A Case Study on Safety Analysis Procedure of Aircraft System using the Relex

  • 이동우 (한국항공대학교 항공전자연구소) ;
  • 김입수 (방위사업청 헬기사업팀) ;
  • 나종화 (한국항공대학교 항공전자연구소)
  • Lee, Dong-Woo (Avionics Research Institute, Korea Aerospace University) ;
  • Kim, Ip-Su (Helicopter Project Team, Defense Acquisition Program Administration) ;
  • Na, Jong-Whoa (Avionics Research Institute, Korea Aerospace University)
  • 투고 : 2018.05.08
  • 심사 : 2018.06.22
  • 발행 : 2018.06.30

초록

항공전자 시스템의 개발할 때 항공 사고를 예방하기 위해서 SAE ARP4761 (민간 항공 시스템 및 장비 안전성 평가 프로세스 수행 방법 및 지침) 규격에 명시된 안전성 분석 및 평가를 수행한다. 안전성 분석은 시스템의 정상상태가 아닌 비정상상태에 대한 지식과 다른 규격들 간의 상호 연관성에 대한 지식이 요구된다. 때문에, 안전인증규격의 준수를 입증하는 자료를 자동으로 출력하는 도구가 필요하다. 본 연구는 규격의 안전성 분석 절차를 도식화하고, 안전 분석 CAD 도구들을 개별 절차에 적용하는 방법을 연구하였다. 예시 연구로서, ARP4761 부록의 여객기용 휠 제동 시스템 (WBS; wheel brake system)을 대상으로 ARP4761분석을 수행하였다.

In developing avionics systems, safety analysis and evaluation specified in SAE ARP4761 (Methods and Guidelines for Civil Aviation System and Equipment Safety Assessment Process) are carried out to prevent air accidents. Safety analysis requires knowledge of the abnormal state of the system, not its normal state, and its interrelationships with other standards. Therefore, a tool that automatically outputs data which proves compliance with safety certification standards is required. In this study,In this study, Schematized the safety analysis procedure of the specification and studied the method of applying the safety analysis CAD tools to individual procedure. As an example study, ARP4761 analysis was performed on the wheel brake system (WBS) of the ARP4761 appendix.

키워드

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