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首页> 外文期刊>Neural Networks and Learning Systems, IEEE Transactions on >Deep Convolutional Identifier for Dynamic Modeling and Adaptive Control of Unmanned Helicopter
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Deep Convolutional Identifier for Dynamic Modeling and Adaptive Control of Unmanned Helicopter

机译:用于无人直升机动态建模和自适应控制的深度卷积标识符

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摘要

Helicopters are complex high-order and timevarying nonlinear systems, strongly coupling with aerodynamic forces, engine dynamics, and other phenomena. Therefore, it is a great challenge to investigate system identification for dynamic modeling and adaptive control for helicopters. In this paper, we address the system identification problem as dynamic regression and propose to represent the uncertainties and the hidden states in the system dynamic model with a deep convolutional neural network. Particularly, the parameters of the network are directly learned from the real flight data of aerobatic helicopter. Since the deep convolutional model has a good performance for describing the dynamic behavior of the hidden states and uncertainties in the flight process, the proposed identifier manifests strong robustness and high accuracy, even for untrained aerobatic maneuvers. The effectiveness of the proposed method is verified by various experiments with the real-world flight data from the Stanford Autonomous Helicopter Project. Consequently, an adaptive flight control scheme including a deep convolutional identifier and a backstepping-based controller is presented. The stability of the flight control scheme is rigorously proved by the Lyapunov theory. It reveals that the tracking errors for both the position and attitude of unmanned helicopter asymptotic converge to a small neighborhood of the origin.
机译:直升机是复杂的高阶和时变非线性系统,与空气动力,发动机动力学和其他现象密切相关。因此,研究用于直升机的动态建模和自适应控制的系统识别是一个巨大的挑战。在本文中,我们将系统识别问题作为动态回归来解决,并提出用深度卷积神经网络来表示系统动态模型中的不确定性和隐藏状态。特别是,从特技直升机的真实飞行数据中直接学习网络的参数。由于深度卷积模型在描述飞行过程中隐藏状态和不确定性的动态行为方面具有良好的性能,因此即使对于未经训练的特技飞行演习,所提出的标识符也表现出强大的鲁棒性和高精度。斯坦福自治直升机项目的实际飞行数据通过各种实验验证了该方法的有效性。因此,提出了一种自适应飞行控制方案,该方案包括一个深度卷积标识符和一个基于反推的控制器。李雅普诺夫理论严格证明了飞行控制方案的稳定性。它表明,无人直升机渐近线的位置和姿态的跟踪误差都收敛于原点的一个小邻域。

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