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