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Nonlinear Flight Control Using Neural Networks and Feedback Linearization

机译:非线性飞行控制使用神经网络和反馈线性化

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Aircraft dynamics are in general nonlinear, time-varying, and may be highly uncertain. Current-generation controllers rely on approximate linearized models of the aircraft and use gain scheduling to accommodate changes in vehicle dynamics as the flight regime varies. The techniques of feedback linearization provide a means of developing invariant controllers that give a desired response in all flight modes. However, the implementation of these techniques involves intensive online computations. The structure imposed by feedback linearization proves an ideal setting for introducing neural networks to the flight-control loop. In this paper, a structure for the use of neural networks to represent the nonlinear inverse transformations needed for feedback linearization is proposed and evaluated. In order to compensate for unmodeled nonlinearities and parameter drifg a second network is introduced which permits online learning. In addition, the paper addresses the robust stability problem in the context of neural-network representation error.
机译:飞机动力学在一般非线性,时变,并且可能是非常不确定的。当前生成控制器依靠飞机的近似线性化模型,并使用增益调度以适应车辆动态的变化,因为飞行制度变化。反馈线性化的技术提供了一种开发不变控制器的方法,该控制器在所有飞行模式中提供所需的响应。但是,这些技术的实现涉及密集的在线计算。反馈线性化施加的结构证明了将神经网络引入飞行控制回路的理想设置。在本文中,提出了一种用于使用神经网络来表示反馈线性化所需的非线性逆变换的结构进行了评估。为了补偿未拼接的非线性和参数DRIFG,介绍了第二网络,其允许在线学习。此外,本文在神经网络表示错误的上下文中解决了鲁棒稳定性问题。

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