Fuzzy control of wing rock for slender delta wings

J. H. Tarn, F. Y. Hsu

Research output: Chapter in Book/Report/Conference proceedingConference contribution

13 Citations (Scopus)

Abstract

It is commonly believed that fuzzy logic control (FLC) has excellent robust characteristics. In this paper, fuzzy logic-based roll controllers are designed to control wing-rock motion of a free-to-roll stinged delta wing. The dynamics of an aircraft is a complex function of the flight conditions. The free-to-roll stinged delta wing provides investigations of these variations as well as the exhibited highly nonlinear dynamics of limit cycle at high angle-of-attack. a rule-base FLC is first designed to suppress wing rock phenomenon. The goal to utilize this type of FLC is to demonstrate the ability of FLC to capture qualitative control strategies and implement highly flexible control behaviors. Then a newly proposed data-base FLC design method is used to improve the performance characteristic to a level compatible with the performance of optimal linear controller locally while maintaining the high performance through the whole flight envelope.

Original languageEnglish
Title of host publicationAmerican Control Conference
PublisherPubl by IEEE
Pages1159-1161
Number of pages3
ISBN (Print)0780308611, 9780780308619
DOIs
Publication statusPublished - 1993
EventProceedings of the 1993 American Control Conference Part 3 (of 3) - San Francisco, CA, USA
Duration: 1993 Jun 21993 Jun 4

Publication series

NameAmerican Control Conference

Other

OtherProceedings of the 1993 American Control Conference Part 3 (of 3)
CitySan Francisco, CA, USA
Period93-06-0293-06-04

All Science Journal Classification (ASJC) codes

  • Electrical and Electronic Engineering

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