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

被引：0

作者：

WooSung-Yeom ^{[1
]}

Seokwun-Ha ^{[2
]}

机构：

[1] Korea Aerosp Ind LTD, Sacheon Si, South Korea

[2] Gyeongsang Natl Univ, Dept Aerosp & Software Engn, Jinju, South Korea

来源：

JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 2020年 / 48卷 / 01期

关键词：

AFCS; OFP; FMET; Stability; Reliability;

D O I：

10.5139/JKSAS.2020.48.1.55

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

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.

引用

页码：55 / 62

页数：8

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