Asymmetric Variable Universe Adaptive Landing Fuzzy Controller for Carrier-Based Aircraft

다국어 초록 (Multilingual Abstract)

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 (Table of Contents)

• 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