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Non-Fragile Static Output Feedback Control Design with Guaranteed Cost of Uncertain Systems with Application to Helicopter System

机译:非易碎静态输出反馈控制设计,具有应用于直升机系统的不确定系统的保证成本

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The paper is concerned with non-fragile control design via output feedback controller for uncertain systems. In control design for physical systems, there are chances that malfunction in actuator happens and an exact value of the control input may not be applied. Hence controller gain variations should be considered in the control design. Additionally, many results on the state feedback control design have been given in the literature. However, in the actual situation, the state of the system is not always measured and the output feedback control design is desired. In this paper, non-fragile guaranteed cost control via output feedback control for uncertain systems is considered and a control design of stabilizing controllers with guaranteed cost and robustness against uncertainties of system parameters and control gains is proposed. The robust stability analysis of the closed-loop system and controller design are given in terms of LMI conditions, which are less conservative than the existing results.
机译:本文涉及通过输出反馈控制器的非脆弱控制设计,用于不确定系统。在对物理系统的控制设计中,有机会发生致动器发生故障,并且可能无法应用控制输入的精确值。因此,控制器增益变化应在控制设计中考虑。另外,在文献中已经给出了州反馈控制设计的许多结果。然而,在实际情况下,不总是测量系统的状态,并且需要输出反馈控制设计。在本文中,考虑了通过输出反馈控制的非脆弱的保证成本控制,并提出了具有保证成本的稳定控制器的控制设计,以及对系统参数的不确定性和控制增益的鲁棒性。闭环系统和控制器设计的稳定稳定性分析在LMI条件方面给出,这些条件不如现有结果保守。

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