Application of linguistic fuzzy neural network to landing control

Li-Hsiang Chien, J. Juang
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Abstract

Most aircraft accidents occurred during the final approach. Wind disturbance is one of the significant factors in these accidents. During the landing phase, the Automatic Landing System (ALS) can help aircraft land safely and significantly reduce the pilot’s work loading. Control schemes of the conventional ALS usually use gain-scheduling and traditional PID control techniques. A traditional controller cannot control the aircraft if the weather conditions are beyond the allowed limits. To improve the performance of the landing control, this study applies a linguistic fuzzy neural network (LFNN) to replace the conventional controller of ALS. Adaptive learning rules are proposed to enhance the LFNN control ability. The method used to obtain adaptive learning rules is the Lyapunov stability theory. Moreover, the convergence of the system performance error is proved by the Lyapunov theory. This study also compares previously proposed control schemes in aircraft landing control. Different turbulence strengths are implemented into the flight simulation to make the proposed controller more robust and adaptive to various wind disturbance conditions. The LFNN controller can successfully overcome 75 ft/s wind speed, while the adaptive LFNN can reach 80 ft/s with optimal learning rates. Using optimal convergence theorems, the proposed controller performs better than the controllers trained by a fixed learning rate.
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语言模糊神经网络在着陆控制中的应用
大多数飞机事故都发生在最后进近过程中。风干扰是造成这些事故的重要因素之一。在着陆阶段,自动着陆系统(ALS)可以帮助飞机安全着陆,并大大减轻飞行员的工作负担。传统自动着陆系统的控制方案通常采用增益调度和传统 PID 控制技术。如果天气条件超出允许范围,传统控制器就无法控制飞机。为了提高着陆控制的性能,本研究采用语言模糊神经网络(LFNN)来替代传统的 ALS 控制器。研究提出了自适应学习规则,以增强 LFNN 的控制能力。获得自适应学习规则的方法是 Lyapunov 稳定性理论。此外,Lyapunov 理论还证明了系统性能误差的收敛性。本研究还比较了之前提出的飞机着陆控制方案。在飞行仿真中实施了不同的湍流强度,以使提出的控制器对各种风干扰条件具有更强的鲁棒性和适应性。LFNN 控制器能成功克服 75 英尺/秒的风速,而自适应 LFNN 则能以最佳学习率达到 80 英尺/秒。利用最优收敛定理,所提出的控制器比采用固定学习率训练的控制器性能更好。
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