Takagi-Sugeno Fuzzy Model-Based Flight Control and Failure Stabilization

This paper presents a Takagi-Sugeno fuzzy model-based approach to modeling, controlling, and stabilizing an aircraft in both normal and damaged conditions. The major contributions of this paper are as follows. First, it introduces the Takagi-Sugeno modeling and the parallel distributed compensation...

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Bibliographic Details
Published in:Journal of guidance, control, and dynamics control, and dynamics, 2011-09, Vol.34 (5), p.1543-1555
Main Authors: Butler, Evan J, Wang, Hua O, Burken, John J
Format: Article
Language:English
Subjects:
Aging aircraft
Aircraft
Applied sciences
Aviation
Compensation
Computer science
control theory
systems
Computer systems and distributed systems. User interface
Control system synthesis
Control theory. Systems
Damage
Exact sciences and technology
Failure
Fuzzy
Fuzzy logic
Mathematical models
Military aircraft
Military planes
Modelling and identification
Neural networks
Software
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Summary:This paper presents a Takagi-Sugeno fuzzy model-based approach to modeling, controlling, and stabilizing an aircraft in both normal and damaged conditions. The major contributions of this paper are as follows. First, it introduces the Takagi-Sugeno modeling and the parallel distributed compensation control approach. Then, it demonstrates how the approach can be applied to aircraft in a systematic manner. Finally, the approach is applied to the modified NASA F-15 number 837 nonlinear model, and preliminary simulation results are presented. The benefits of using a Takagi-Sugeno model-based parallel distributed compensation control approach include a systematic controller design procedure, mathematical proof of stability for classes of failures, and intuitive insight into damage effects on an aircraft. This work is the first to present this control approach as applied to aircraft. [PUBLISHER ABSTRACT]
ISSN:0731-5090
1533-3884
DOI:10.2514/1.52509