NDLI: Fuzzy logic in restructurable flight control systems

Content Provider	IEEE Xplore Digital Library
Author	Ho, H.S. Balakrishnan, S.N.
Copyright Year	1995
Description	Author affiliation: Dept. of Mech. & Aerosp. Eng., Missouri Univ., Rolla, MO, USA (Ho, H.S.; Balakrishnan, S.N.)
Abstract	In this paper, a fuzzy logic controller (FLC) is proposed for restructurable flight control systems. The role of the FLC is to stabilize the aircraft upon a fault occurrence. The FLC derives pitch/roll/yaw controls from a generic knowledge base characterized by 49 if-then rules. A linearized model representative of a modern jet fighter provides the basis for the numerical simulation. Simulated faults include various degrees of surface loss at the right stabilator, combined with reduced ailerons and rudder control power. The FLC accomplishes the stabilization task under test conditions without any knowledge of the system parameters. The numerical results demonstrate the potential of the FLC as a suitable control algorithm that bridges the critical gap between the fault occurrence and the full implementation of the new control law.
Starting Page	1362
Ending Page	1366
File Size	439711
Page Count	5
File Format	PDF
ISBN	0780324455
DOI	10.1109/ACC.1995.520973
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	1995-06-21
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Fuzzy logic Aerospace control Control systems Aircraft Size control Fault detection Nonlinear control systems Aerospace engineering Performance loss Control system synthesis
Content Type	Text
Resource Type	Article

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4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
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