Fuzzy control of wing rock for slender delta wings

Jiun-Haur Tarn, F. Y. Hsu

研究成果: Conference contribution

3 引文 (Scopus)

摘要

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 flight conditions. The free-to-roll stinged delta wing permits investigation of these variations, as well as the highly nonlinear dynamics of limit cycle at high angle-of-attack. A rule-base fuzzy logic control (FLC) is designed to suppress wing rock phenomena. The goal is to demonstrate the ability of FLC to capture qualitative control strategies and implement highly flexible control behaviors. A database FLC design method is used to improve performance characteristics to a level compatible with the performance of an optimal linear controller while maintaining high performance throughout the whole flight envelope.

原文English
主出版物標題TENCON 1992 - Technology Enabling Tomorrow
主出版物子標題Computers, Communications and Automation towards the 21st Century - 1992 IEEE Region 10 International Conference
發行者Institute of Electrical and Electronics Engineers Inc.
頁面715-719
頁數5
ISBN(電子)0780308492
DOIs
出版狀態Published - 1992 一月 1
事件1992 IEEE Region 10 International Conference on Technology Enabling Tomorrow: Computers, Communications and Automation towards the 21st Century, TENCON 1992 - Melbourne, Australia
持續時間: 1992 十一月 111992 十一月 13

出版系列

名字IEEE Region 10 Annual International Conference, Proceedings/TENCON
ISSN(列印)2159-3442
ISSN(電子)2159-3450

Conference

Conference1992 IEEE Region 10 International Conference on Technology Enabling Tomorrow: Computers, Communications and Automation towards the 21st Century, TENCON 1992
國家Australia
城市Melbourne
期間92-11-1192-11-13

指紋

Fuzzy control
Rocks
Fuzzy logic
Flight envelopes
Controllers
Angle of attack
Aircraft

All Science Journal Classification (ASJC) codes

  • Computer Science Applications
  • Electrical and Electronic Engineering

引用此文

Tarn, J-H., & Hsu, F. Y. (1992). Fuzzy control of wing rock for slender delta wings. 於 TENCON 1992 - Technology Enabling Tomorrow: Computers, Communications and Automation towards the 21st Century - 1992 IEEE Region 10 International Conference (頁 715-719). [271877] (IEEE Region 10 Annual International Conference, Proceedings/TENCON). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/TENCON.1992.271877
Tarn, Jiun-Haur ; Hsu, F. Y. / Fuzzy control of wing rock for slender delta wings. TENCON 1992 - Technology Enabling Tomorrow: Computers, Communications and Automation towards the 21st Century - 1992 IEEE Region 10 International Conference. Institute of Electrical and Electronics Engineers Inc., 1992. 頁 715-719 (IEEE Region 10 Annual International Conference, Proceedings/TENCON).
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Tarn, J-H & Hsu, FY 1992, Fuzzy control of wing rock for slender delta wings. 於 TENCON 1992 - Technology Enabling Tomorrow: Computers, Communications and Automation towards the 21st Century - 1992 IEEE Region 10 International Conference., 271877, IEEE Region 10 Annual International Conference, Proceedings/TENCON, Institute of Electrical and Electronics Engineers Inc., 頁 715-719, 1992 IEEE Region 10 International Conference on Technology Enabling Tomorrow: Computers, Communications and Automation towards the 21st Century, TENCON 1992, Melbourne, Australia, 92-11-11. https://doi.org/10.1109/TENCON.1992.271877

Fuzzy control of wing rock for slender delta wings. / Tarn, Jiun-Haur; Hsu, F. Y.

TENCON 1992 - Technology Enabling Tomorrow: Computers, Communications and Automation towards the 21st Century - 1992 IEEE Region 10 International Conference. Institute of Electrical and Electronics Engineers Inc., 1992. p. 715-719 271877 (IEEE Region 10 Annual International Conference, Proceedings/TENCON).

研究成果: Conference contribution

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AB - 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 flight conditions. The free-to-roll stinged delta wing permits investigation of these variations, as well as the highly nonlinear dynamics of limit cycle at high angle-of-attack. A rule-base fuzzy logic control (FLC) is designed to suppress wing rock phenomena. The goal is to demonstrate the ability of FLC to capture qualitative control strategies and implement highly flexible control behaviors. A database FLC design method is used to improve performance characteristics to a level compatible with the performance of an optimal linear controller while maintaining high performance throughout the whole flight envelope.

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Tarn J-H, Hsu FY. Fuzzy control of wing rock for slender delta wings. 於 TENCON 1992 - Technology Enabling Tomorrow: Computers, Communications and Automation towards the 21st Century - 1992 IEEE Region 10 International Conference. Institute of Electrical and Electronics Engineers Inc. 1992. p. 715-719. 271877. (IEEE Region 10 Annual International Conference, Proceedings/TENCON). https://doi.org/10.1109/TENCON.1992.271877