基于干扰观测器的飞行仿真转台全局滑模控制方法

Global Sliding Mode Control Method for a Flight Simulator Based on Disturbance Observer

  • 摘要: 针对飞行仿真转台容易受到外界干扰和参数变化影响的特点,提出了一种基于干扰观测器(DOB)的全局滑模控制 (GSMC) 方法.采用一个积分切换函数使系统的初始状态即位于滑模面上,解决了到达阶段的问题,并且设计的控制器保证了系统的整个响应过程具有全局滑模特性.为减小控制量中抖振的影响,引入了干扰观测器作为干扰补偿环节.加入干扰观测器后切换增益只需要大于干扰估计误差的上界.实验表明,本文提出的控制方法针对飞行仿真转台系统的不确定性具有很强的鲁棒性,能有效地抑制控制量中的抖振,并具有良好的跟踪性能.

     

    Abstract: Flight simulators are susceptible to external disturbance and parameter variation. To solve this problem, we propose a global sliding mode control (GSMC) method based on the disturbance observer (DOB) for the flight simulator. We use an integral switching function to set the initial state of the system on the sliding surface in order to solve the reaching phase problem. Then we design the sliding mode controller to guarantee the global sliding mode property. To suppress chattering in control input, we introduce a disturbance compensation part based on DOB. Then the switching gain only needs to be greater than the upper bound of disturbance estimation error. Experimental results show that the proposed method possesses strong robustness against uncertainties, great chattering suppression in control input, and good tracking performance.

     

/

返回文章
返回