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
Link To Document :
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