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http://dx.doi.org/10.5139/JKSAS.2020.48.1.55

Method of Conducting and Verification for Failure Mode Effect Test of Rotary Automatic Flight Control System Software  

Yeom, WooSung (Korea Aerospace Industries, LTD)
Ha, Seokwun (Department of Aerospace and Software Engineering, Gyeongsang National University)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.48, no.1, 2020 , pp. 55-62 More about this Journal
Abstract
It is necessary to develop digital flight control system by digital control technology to ensure stability and maneuverability of rotary helicopter. It is important to meet functional requirements of helicopter flight control system OFP and verify system reliability directly linked to flight safety as a core technology that avoids the transfer of technology by overseas advanced helicopter manufacturer. In this paper, we studied how to perform FMET for operational flight program of rotary automatic flight control system.
Keywords
AFCS; OFP; FMET; Stability; Reliability;
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  • Reference
1 MIL-HDBK-516C, "Airworthiness Certification Criteria," February 2008, p. 149.
2 MIL-HDBK-87213A, "Electronically/Optically Generated Airborne Displays," February 2005, p. 16.
3 EUROCOPTER, "AFCS Description Document," Rev F, January 2011, p. 36.
4 Kim, C., "5 Design Evaluation of Safety-Critical Computer Systems," Electrical and Computer Engineering Howard University, May 2008, p. 3.
5 Yeom, W. S., "Core-Tech AFCS System Test Plan," Korea Aerospace Industry, September 2017, p. 5.
6 Kim, H. S., "Core-Tech Automatic Flight Control System Test Description," Korea Aerospace Industry, January 2018, p. 10.
7 Yeom, W. S., "Core-Tech Automatic Flight Control System Test Description Appendix C," Korea Aerospace Industry, July 2018, pp. 15, 18.