Incremental Model-Based Heuristic Dynamic Programming with Output Feedback Applied to Aerospace System Identification and Control

Bo Sun, E. Kampen
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引用次数: 3

Abstract

Sufficient information about system dynamics and inner states is often unavailable to aerospace system controllers, which requires model-free and output feedback control techniques, respectively. This paper presents a novel self-learning control algorithm to deal with these two problems by combining the advantages of heuristic dynamic programming and incremental modeling. The system dynamics is completely unknown and only input/output data can be acquired. The controller identifies the local system models and learns control polices online both by tuning the weights of neural networks. The novel method has been applied to a multi-input multi-output nonlinear satellite attitude tracking control problem. The simulation results demonstrate that, compared with the conventional actor-critic-identifier-based heuristic dynamic programming algorithm with three networks, the proposed adaptive control algorithm improves online identification of the nonlinear system with respect to precision and speed of convergence, while maintaining similar performance compared to the full state feedback situation.
基于增量模型的输出反馈启发式动态规划在航天系统辨识与控制中的应用
航空航天系统控制器通常无法获得关于系统动力学和内部状态的充分信息,这分别需要无模型和输出反馈控制技术。本文结合启发式动态规划和增量建模的优点,提出了一种新的自学习控制算法来解决这两个问题。系统动力学是完全未知的,只能获得输入/输出数据。控制器通过调整神经网络的权值来识别局部系统模型并在线学习控制策略。该方法已应用于多输入多输出非线性卫星姿态跟踪控制问题。仿真结果表明,与传统的基于关键标识符的三网络启发式动态规划算法相比,本文提出的自适应控制算法在提高非线性系统在线辨识精度和收敛速度的同时,保持了与全状态反馈情况相似的性能。
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