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Neural Network-Based Optimal Adaptive Output Feedback Control of a Helicopter UAV

机译:基于神经网络的直升机无人机自适应输出反馈最优控制

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摘要

Helicopter unmanned aerial vehicles (UAVs) are widely used for both military and civilian operations. Because the helicopter UAVs are underactuated nonlinear mechanical systems, high-performance controller design for them presents a challenge. This paper introduces an optimal controller design via an output feedback for trajectory tracking of a helicopter UAV, using a neural network (NN). The output-feedback control system utilizes the backstepping methodology, employing kinematic and dynamic controllers and an NN observer. The online approximator-based dynamic controller learns the infinite-horizon Hamilton–Jacobi–Bellman equation in continuous time and calculates the corresponding optimal control input by minimizing a cost function, forward-in-time, without using the value and policy iterations. Optimal tracking is accomplished by using a single NN utilized for the cost function approximation. The overall closed-loop system stability is demonstrated using Lyapunov analysis. Finally, simulation results are provided to demonstrate the effectiveness of the proposed control design for trajectory tracking.
机译:直升机无人飞行器(UAV)被广泛用于军事和民用行动。由于直升机无人机是欠驱动的非线性机械系统,因此针对其的高性能控制器设计提出了挑战。本文通过使用神经网络(NN)的直升机无人飞行器的轨迹跟踪,通过输出反馈引入了最优控制器设计。输出反馈控制系统利用反推方法,采用运动学和动态控制器以及一个NN观察器。基于在线近似器的动态控制器在连续时间内学习无限地平线的Hamilton–Jacobi–Bellman方程,并通过最小化成本函数(时间提前)来计算相应的最佳控制输入,而无需使用值和策略迭代。最佳跟踪是通过使用用于成本函数逼近的单个NN来完成的。使用Lyapunov分析证明了整个闭环系统的稳定性。最后,提供仿真结果以证明所提出的轨迹跟踪控制设计的有效性。

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