Design of EMP Test Software of Flight Control Computer

被引：0

作者：

Zhou Chunmei ^{[1
]}

Zhang Chunxia ^{[1
]}

Dong Wenjie ^{[1
]}

Zhang Jun ^{[1
]}

Lin Jinyong ^{[1
]}

机构：

[1] Beijing Aerosp Automat Control Inst, Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing, Peoples R China

来源：

PROCEEDINGS OF THE 2012 SECOND INTERNATIONAL CONFERENCE ON INSTRUMENTATION & MEASUREMENT, COMPUTER, COMMUNICATION AND CONTROL (IMCCC 2012) | 2012年

关键词：

Flight Control Computer; EMP; Test; Software;

D O I：

10.1109/IMCCC.2012.356

中图分类号：

TP301 [理论、方法];

学科分类号：

081202 ;

摘要：

As the core device of Aircraft Control System, under the severe environment full of EMP, flight control computer would occur transient faults by interference of EMP, even cause mission failure. It's essential for a flight control computer in designing damage mode test software of EMP, locating faults, registering and analyzing fault information. This paper will introduce test flow and test scheme, gives test software flow, and then validates the feasibility of software by experimentation.

引用

页码：1522 / 1525

页数：4

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