Design of EMP Test Software of Flight Control Computer

Author

Zhou Chunmei ; Zhang Chunxia ; Dong Wenjie ; Zhang Jun ; Lin Jinyong

Author_Institution

Nat. Key Lab. of Sci. & Technol. on Aerosp. Intell. Control, Beijing Aerosp. Autom. Control Inst., Beijing, China

fYear

2012

fDate

8-10 Dec. 2012

Firstpage

1522

Lastpage

1525

Abstract

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.

Keywords

aerospace computing; aerospace control; aerospace testing; control engineering computing; electromagnetic interference; electromagnetic pulse; fault location; EMP interference; EMP test software; aircraft control system; damage mode test software design; fault information analysis; flight control computer; transient fault location; Aerospace control; Aerospace testing; Computer crashes; Computers; Software; Timing; Transient analysis; EMP; Flight Control Computer; Software; Test;

fLanguage

English

Publisher

ieee

Conference_Titel

Instrumentation, Measurement, Computer, Communication and Control (IMCCC), 2012 Second International Conference on

Conference_Location

Harbin

Print_ISBN

978-1-4673-5034-1

Type

conf

DOI

10.1109/IMCCC.2012.356

Filename

6429192