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Adaptive neural observer-based backstepping fault tolerant control for near space vehicle under control effector damage

机译:控制效应器损伤下基于自适应神经观测器的反步容错控制

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摘要

In this study, a theoretical framework for reconfigurable flight control is developed and applied to near space vehicle (NSV) attitude dynamics. First, NSV reentry mode is described. Second, an adaptive neural network observer is proposed, which ensures asymptotic convergence of the state observer error to zero under control effector damage and uncertainty. Next, a reconfigurable command-filter backstepping controller is designed based on the adaptive neural network observer. The authors focus is on the accommodation of the control effector damage, uncertainty and resulting disturbances. It is shown that the presented new control design results in asymptotic convergence of the attitude tracking error to zero. Finally, simulation results are given to demonstrate the effectiveness and potential of the proposed fault tolerant control scheme.
机译:在这项研究中,可重构飞行控制的理论框架被开发并应用于近太空飞行器(NSV)姿态动力学。首先,描述NSV再进入模式。其次,提出了一种自适应神经网络观测器,该观测器可确保在控制效应器损坏和不确定性的情况下,状态观测器误差渐近收敛至零。接下来,基于自适应神经网络观察器设计了可重构的命令过滤器反推控制器。作者的重点是控制效应器损坏,不确定性和由此产生的干扰的调节。结果表明,提出的新控制设计导致姿态跟踪误差渐近收敛于零。最后,仿真结果证明了所提出的容错控制方案的有效性和潜力。

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