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Adaptive neural flight control system for helicopter

机译:直升机的自适应神经飞行控制系统

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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.
机译:本文提出了一种用于执行非线性机动的直升机的自适应神经飞行控制设计。该控制策略使用神经控制器来辅助现有的常规控制器。神经控制器使用实时学习的动态径向基函数网络,该网络使用结合了神经元生长准则的基于Lyapunov的在线更新规则。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实现网络。拟议的自适应法则提供了必要的全局稳定性和更好的跟踪性能。使用非线性桌面仿真模型进行仿真研究。所提出的自适应控制机制的性能清楚地表明,当直升机执行非线性机动时,它是非常有效的。

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