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Method of Conducting and Verification for Failure Mode Effect Test of Rotary Automatic Flight Control System Software
- Authors
- WooSung-Yeom; Seokwun-Ha
- Issue Date
- Jan-2020
- Publisher
- 한국항공우주학회
- Keywords
- AFCS; OFP; FMET; Stability; Reliability
- Citation
- Journal of The Korean Society Aeronautical and Space Sciences, v.48, no.1, pp 55 - 62
- Pages
- 8
- Indexed
- SCOPUS
ESCI
KCI
- Journal Title
- Journal of The Korean Society Aeronautical and Space Sciences
- Volume
- 48
- Number
- 1
- Start Page
- 55
- End Page
- 62
- ISSN
- 1225-1348
2287-6871
- 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.
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