Earticle

초록

영어

During the process of aircraft landing, the control manners of carrier-based aircraft are always used to study. This is one of the important ways to avoid pilot-aircraft adverse coupling. In order to keep the accuracy of landing, this paper presents an improved asymmetric variable universe adaptive landing fuzzy controller with Safe Flight Area during approach for carrier-based aircraft. By means of universe-conversion factors and contraction–expansion factors, universe of discourse can be modified online, and fuzzy rules can reproduce automatically to adapt to the modified universe of discourse. The model simulation results indicate the better performance of the new method in comparison with the traditional controller with more accuracy and practicability.

목차

Abstract
 1. Introduction
 2. Asymmetric Variable Universe Adaptive Fuzzy Controller
  2.1. Design Universe-conversion Factors
  2.2. Design Contraction-expansion Factors
  2.3. Design Control Algorithm of Asymmetric Variable Universe Fuzzy System
 3. Safe Flight Area of Carrier-based Aircraft
 4. Model Simulation
 6. Conclusion
 Acknowledgement
 References

키워드

저자

• Hui Li [ School of Computer and Information Engineering Harbin University of Commerce ]
• Xiao-dong Su [ School of Computer and Information Engineering Harbin University of Commerce ]
• Hai-tao Jiang [ School of Computer and Information Engineering Harbin University of Commerce ]

참고문헌

발행기관

간행물

표지보기 관심저널 등록

• 간행물명

  International Journal of Smart Home

• 간기

  격월간

• pISSN

  1975-4094

• 수록기간

  2008~2016

• 십진분류

  KDC 505 DDC 605