高超声速飞行器姿态控制的深度FBSDE控制器

Yujun Liu, Yutian Wang, Zeyan Zhuang, Xian Guo
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引用次数: 1

摘要

高超声速飞行器的姿态控制由于系统的不确定性和各种噪声,是一个非常具有挑战性的课题。在本文中,我们提出了一种新的方法来解决这个问题。首先,将高超声速飞行器的姿态控制重新表述为一个正反向随机微分方程系统。利用深度神经网络(Deep Neural Networks, dnn)求解方程的最优解。我们研究了几种深度神经网络,包括基于fc的体系结构和基于lstm的体系结构,并提出了一种新的基于fc的体系结构,该体系结构在不同的时间步长之间共享权值,在该问题中表现良好。在无约束和控制约束两种情况下对算法的性能和通用性进行了测试。仿真和实验结果验证了该算法的优越性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Deep FBSDE Controller for Attitude Control of Hypersonic Aircraft
Attitude control of Hypersonic Aircraft is a very challenging subject due to the uncertainties and various noises of the system. In this paper, we propose a new methodology to solve this problem. Firstly, the attitude control of Hypersonic Aircraft is reformulated as a system of Forward-Backward Stochastic Differential Equations. Deep Neural Networks (DNNs) are used to get optimal solution of the equations. We have studied several deep neural networks, including FC-based architecture and LSTM-based architecture and proposed a new FC-based architecture that shares the weights between different time steps, which performed satisfactorily in this problem. The performance and universality of the algorithm are tested in both unconstrained and control-constrained cases. Simulation and experimental results verify the superiority of the algorithm.
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