DocumentCode
332566
Title
Failure tolerance of sensors in flight control systems in electromagnetic environment
Author
Suh, Jon ; Chang, B.C. ; Lau, A.C.
Author_Institution
Dept. of Mech. Eng., Drexel Univ., Philadelphia, PA, USA
Volume
1
fYear
1998
fDate
31 Oct-7 Nov 1998
Abstract
High Intensity Radiated Field (HIRE) conditions may cause sensor and/or controller failure in flight control system. In this paper, a flight dynamics imitation scheme is proposed to establish the failure tolerance of sensors in Electro-Magnetic Environment (EME)
Keywords
avionics; electric sensing devices; electromagnetic interference; failure analysis; avionics; electromagnetic environment; electronic sensors; failure tolerance; flight control systems; flight dynamics imitation scheme; high intensity radiated field; Aerospace control; Aerospace electronics; Control systems; Interference; Mechanical sensors; Military aircraft; Pollution measurement; Radio frequency; Sensor systems; Stability;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1998. Proceedings., 17th DASC. The AIAA/IEEE/SAE
Conference_Location
Bellevue, WA
Print_ISBN
0-7803-5086-3
Type
conf
DOI
10.1109/DASC.1998.741551
Filename
741551
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