DocumentCode :
2674219
Title :
Reconfiguration of flight control systems for actuator failures
Author :
Bajpai, G. ; Chang, B.C. ; Lau, A.
Author_Institution :
Dept. of Mech. Eng. & Mech., Drexel Univ., Philadelphia, PA, USA
Volume :
1
fYear :
2000
fDate :
2000
Abstract :
We consider the problem of designing fault tolerant control for transient failures in the flight control system caused by harsh electromagnetic environments. We examine principles of fault tolerant design, and discuss integrated local supervisory control of these systems. As an example, we present a sample design of a control mixer to achieve fault tolerance in the event of failures in the actuators
Keywords :
actuators; aircraft computers; aircraft control; control nonlinearities; control system analysis computing; directed graphs; electromagnetic interference; fault tolerant computing; redundancy; state-space methods; EMI; actuator failures; closed loop; control mixer; digital upsets; directed graph representation; fault isolation; fault tolerant control design; fault tolerant microprocessors; flight control systems reconfiguration; fly-by-wire aircraft; global coordinator; harsh electromagnetic environments; integrated local supervisory control; logic changes; nonlinearities; redundancy; state-space equations; transient failures; Actuators; Aerospace control; Aerospace electronics; Aircraft; Control systems; Electromagnetic radiation; Electromagnetic transients; Fault tolerance; Fault tolerant systems; Logic circuits;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 2000. Proceedings. DASC. The 19th
Conference_Location :
Philadelphia, PA
Print_ISBN :
0-7803-6395-7
Type :
conf
DOI :
10.1109/DASC.2000.886932
Filename :
886932
Link To Document :
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