直升机自适应神经飞行控制系统

S. Suresh
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引用次数: 7

摘要

提出了一种针对直升机非线性机动的自适应神经飞行控制设计方法。该控制策略使用神经控制器辅助现有的传统控制器。神经控制器采用实时学习的动态径向基函数网络,该网络采用基于Lyapunov的在线更新规则与神经元生长准则相结合。实时学习动态径向基函数网络不需要先验训练,也可以找到一个紧凑的网络来实现。所提出的自适应律提供了必要的全局稳定性和较好的跟踪性能。仿真研究采用非线性桌面仿真模型进行。仿真结果表明,所提出的自适应控制机制在直升机进行非线性机动时是非常有效的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Adaptive neural flight control system for helicopter
This paper presents an adaptive neural flight control design for helicopters performing nonlinear maneuver. The control strategy uses a neural controller aiding an existing conventional controller. The neural controller uses a real-time learning dynamic radial basis function network, which uses Lyapunov based on-line update rule integrated with the neuron growth criterion. The real-time learning dynamic radial basis function network does not require a priori training and also find a compact network for implementation. The proposed adaptive law provide necessary global stability and better tracking performance. The simulation studies are carried-out using a nonlinear desktop simulation model. The performances of the proposed adaptive control mechanism clearly show that it is very effective when the helicopter is performing nonlinear maneuver.
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