输出约束下航天推进系统有限时间自适应模糊控制

Finite-Time Adaptive Fuzzy Control for Aerospace Propulsion Systems with Output Constraints

  • 摘要: 本文针对在航天推进气动伺服系统中的双杆气缸,提出了一种基于状态观测器的有限时间自适应模糊控制方法. 尽管关于自适应模糊控制理论已有大量研究,但在气缸控制中同时考虑电压饱和与输出约束的工作尚属首次. 根据模糊逻辑系统原理,本文设计了一种状态观测器,用于估计气动双杆气缸中不可测的状态变量. 基于反步法,构建了输出反馈控制器,并利用障碍Lyapunov函数处理输出约束问题. 本文搭建了包含双杆气缸的试验平台,验证了闭环系统中所有信号均有界,且输出满足约束条件. 试验结果表明,在正弦信号跟踪任务中,该方法的控制精度可达0.1 mm,充分证明了此方法的有效性.

     

    Abstract: This article proposes a finite-time adaptive fuzzy control method based on state observers for the dual-rod cylinder in the aerospace propulsion servo system. Despite considerable research on the theory of adaptive fuzzy control, both voltage saturation and output constraint have not yet been considered simultaneously in pneumatic cylinder control. According to fuzzy logic system, a state observer is designed to estimate the unmeasurable states in the pneumatic dual-rod cylinder. An output feedback controller is developed based on backstepping scheme and the output constraint is handled via the barrier Lyapunov functions. The paper sets up an experimental platform based on a dual-rod cylinder and demonstrates that all closed-loop signals are bounded, and the output remains within the constrained set. Experiment results which achieve an accuracy of 0.1mm for sinusoidal tracking verify the effectiveness of the proposed method.

     

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