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Launch Vehicle Discrete-Time Optimal Tracking Control using Global Dual Heuristic Programming

机译:使用全局双重启发式编程的运载火箭离散时间最优跟踪控制

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Optimal tracking is a widely researched control problem, but the unavailability of sufficient information referring to system dynamics brings challenges. In this paper, an optimal tracking control method is proposed for an unknown launch vehicle based on the global dual heuristic programming technique. The nonlinear system dynamics is identified by an offline trained neural network and a feedforward neuro-controller is developed to obtain the desired system input and to facilitate the execution of the feedback controller. By transforming the tracking control problem into a regulation problem, an iterative adaptive dynamic programming algorithm, subject to global dual heuristic programming with explicit analytical calculations, is utilized to deal with the newly built regulation problem. The simulation results demonstrate that the developed method can learn an effective control law for the given optimal tracking control tasks.
机译:最优跟踪是一个广泛研究的控制问题,但是缺乏有关系统动力学的足够信息会带来挑战。本文提出了一种基于全局双重启发式编程技术的未知运载火箭最优跟踪控制方法。通过离线训练的神经网络识别非线性系统动力学,并开发前馈神经控制器以获得所需的系统输入并促进执行反馈控制器。通过将跟踪控制问题转化为规则问题,利用经过全局双重启发式编程和显式解析计算的迭代自适应动态规划算法来处理新建的规则问题。仿真结果表明,对于给定的最优跟踪控制任务,该方法可以学习有效的控制律。

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