DocumentCode :
1125081
Title :
Multiple Fuzzy Reference Model Adaptive Controller Design for Pitch-Rate Tracking
Author :
Kamalasadan, Sukumar ; Ghandakly, Adel A.
Author_Institution :
West Florida Univ., Pensacola
Volume :
56
Issue :
5
fYear :
2007
Firstpage :
1797
Lastpage :
1808
Abstract :
A multiple fuzzy reference model adaptive controller (MFRMAC) is proposed for nonlinear aircraft pitch-rate tracking. The controller is developed using a direct model reference adaptive control (MRAC) scheme with variable fuzzy logic reference model. The proposed controller provides a soft reference model switching for the multiple modes of operation of the aircraft without any prohibitive computation or explicit system identification. The effectiveness of the technique is assessed by simulation studies based on a 6-DOF high-performance fighter aircraft model undergoing pitch-rate control at a wide range of operating contingencies. It is demonstrated that the scheme performs extremely well when controlling multimodal dynamic systems, as opposed to conventional MRAC designs.
Keywords :
aircraft control; fuzzy control; military aircraft; model reference adaptive control systems; tracking; 6-DOF fighter aircraft model; direct model reference adaptive control; high-performance fighter aircraft model; multimodal dynamic systems; multiple fuzzy reference model adaptive controller design; nonlinear aircraft pitch-rate tracking; pitch-rate control; pitch-rate tracking; soft reference model switching; variable fuzzy logic reference model; Adaptive control; Aerospace control; Aircraft; Control systems; Fuzzy control; Fuzzy logic; Fuzzy systems; Heuristic algorithms; Programmable control; Switches; Fuzzy reference model generation; multiple fuzzy reference model adaptive controller; pitch-rate tracking;
fLanguage :
English
Journal_Title :
Instrumentation and Measurement, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9456
Type :
jour
DOI :
10.1109/TIM.2007.904550
Filename :
4303415
Link To Document :
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