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Robust stabilization of input-delayed systems with design example for rocket motor control

机译:输入延迟系统的鲁棒稳定和火箭发动机控制的设计实例

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摘要

Purpose - This paper aims to use a new design approach based on a Lagrange mean value theorem for the stabilization of multivariable input-delayed system by linear controller. Design/methodology/approach - The delay-dependent asymptotical stability conditions are derived by using augmented Lyapunov-Krasovskii functionals and formulated in terms of conventional Lyapunov matrix equations and some simple matrix inequalities. Proposed design approach is extended to robust stabilization of multi-variable input-delayed systems with unmatched parameter uncertainties. The maximum upper bound of delay size is computed by using a simple optimization algorithm. Findings - A liquid monopropellant rocket motor with a pressure feeding system is considered as a numerical design example. Design example shows the effectiveness of the proposed design approach. Research limitations/implications - The proposed approach can be used in the analysis and design of the uncertain multivariable time-delay systems. Originality/value - The paper has a great potential in the stability analysis of time-delay systems and design of time-delay controllers and may openup a new direction in this area.
机译:目的-本文旨在使用一种基于拉格朗日均值定理的新设计方法,通过线性控制器来稳定多变量输入延迟系统。设计/方法/方法-通过使用增强的Lyapunov-Krasovskii泛函导出延迟相关的渐近稳定性条件,并根据常规Lyapunov矩阵方程和一些简单的矩阵不等式来表示。拟议的设计方法扩展到具有不确定性参数不确定性的多变量输入延迟系统的鲁棒稳定。延迟大小的最大上限是通过使用简单的优化算法来计算的。研究结果-具有压力馈送系统的液体单推进火箭发动机被认为是数值设计实例。设计实例说明了所提出设计方法的有效性。研究局限/意义-所提出的方法可以用于不确定的多变量时滞系统的分析和设计。原创性/价值-本文在时滞系统的稳定性分析和时滞控制器的设计方面具有巨大的潜力,并可能在这一领域开辟新的方向。

著录项

  • 来源
  • 作者

    Elbrous M. Jafarov;

  • 作者单位

    Elbrous M. Jafarov, Department of Aeronautical and Astronautical Engineering, Istanbul Technical University, Istanbul, Turkey;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 23:18:42

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