Title :
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
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;
Conference_Titel :
Instrumentation, Measurement, Computer, Communication and Control (IMCCC), 2012 Second International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4673-5034-1
DOI :
10.1109/IMCCC.2012.356
