柔性翼飞行器的余态逼近强化学习解

M. Abouheaf, W. Gueaieb
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引用次数: 2

摘要

为了实时解决最优控制问题,提出了一种基于协态函数逼近的在线自适应学习方法。提出的方法解决了经典的双启发式动态规划技术在不确定动态环境中的主要问题。它采用策略迭代范式以及自适应批评来实现自适应学习解决方案。所得到的框架不需要或不需要系统动力学的先验知识,这使得它适用于具有高建模不确定性的系统。作为概念验证,将所提出的结构应用于具有未知动力学的柔性翼飞行器的自动驾驶控制,该飞行器在每个纵倾速度条件下都是连续变化的。数值仿真结果表明,自适应控制技术能够在较短的时间内学习系统的动态特性,并对系统状态进行调节。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Reinforcement Learning Solution with Costate Approximation for a Flexible Wing Aircraft
An online adaptive learning approach based on costate function approximation is developed to solve an optimal control problem in real time. The proposed approach tackles the main concerns associated with the classical Dual Heuristic Dynamic Programming techniques in uncertain dynamical environments. It employs a policy iteration paradigm along with adaptive critics to implement the adaptive learning solution. The resultant framework does not need or require prior knowledge of the system dynamics, which makes it suitable for systems with high modeling uncertainties. As a proof of concept, the suggested structure is applied for the auto-pilot control of a flexible wing aircraft with unknown dynamics which are continuously varying at each trim speed condition. Numerical simulations showed that the adaptive control technique was able to learn the system's dynamics and regulate its states as desired in a relatively short time.
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