The anti-windup controller design for multi-propeller aerostat based on nested saturation function

D. Sun, Li Chen, Guochang Zhang, Y. Wen, K. Liang, Xiaoliang Wang
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引用次数: 2

Abstract

This paper proposes two methods to describe the actuator amplitude and rate constraints with nested saturation function. The dynamic model of aerostat in the horizontal plane is established, and then the three order nested saturation controller is designed based on the nested saturation function. And as a result, the amplitude and rate of the actuator output are limited by the amplitude constraints of the nested function and the effectiveness of the control law is verified by simulation. The control quality is guaranteed by the state feedback controller. The advantage of the method is that the controller is simple and has strong ability to suppress disturbance.
基于嵌套饱和函数的多螺旋桨浮空器防卷绕控制器设计
本文提出了用嵌套饱和函数描述执行器振幅和速率约束的两种方法。建立了浮空器在水平面上的动力学模型,并基于嵌套饱和函数设计了三阶嵌套饱和控制器。利用嵌套函数的幅值约束对执行器的输出幅值和速率进行限制,并通过仿真验证了控制律的有效性。通过状态反馈控制器保证控制质量。该方法的优点是控制器简单,抑制干扰的能力强。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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