首页 | 官方网站   微博 | 高级检索  
     

基于嵌套饱和的输入约束浮空器非线性控制
作者姓名:孙丁山  陈丽  温余彬  段登平
作者单位:上海交通大学航空航天学院,上海,200240;上海工程技术大学航空运输学院,上海,201620
基金项目:国家自然科学基金资助项目(61733017);上海浦江人才计划资助项目(18PJD018)
摘    要:提出用嵌套饱和函数描述的控制律形式,可以同时解决速率和幅值约束的控制问题.建立浮空器的三自由度模型,将除螺旋桨推力外的其他作用力作为扰动项,进而把该系统化为类积分链式系统;基于嵌套饱和控制理论,研究了类积分链式系统的控制输入幅值及速率约束与控制器饱和函数参数的关系;以浮空器为研究对象,进行纵向和横向通道解耦控制器设计,实现控制系统输入的幅值和速率有界.利用Lyapunov稳定性原理证明了系统的全局稳定性,分析了可调控制器参数对改善系统的动态性能的影响,在考虑风扰动的情况下,仿真验证了控制器的有效性和鲁棒性. 

关 键 词:多螺旋桨组合浮空器  抗饱和控制器  嵌套饱和函数  幅值及速率约束  微分有界控制器
收稿时间:2017-11-13

Nonlinear control of aerostat with input constraints based on nested saturation
Affiliation:1) School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China2) School of Air Transportation, Shanghai University of Engineering Science, Shanghai 201620, China
Abstract:The propellers of an aerostat are prone to both amplitude and rate saturations during the movement of the aerostat, thus affecting the stability and movement of the system. Generally, the conventional method of processing saturation can only handle the amplitude saturation of the system input, and the rate saturation problem is usually converted to an amplitude saturation problem, so it is a complex process. Therefore, it is worthwhile to study the control method that can simultaneously deal with amplitude and rate saturations. Some anti-windup compensator design methods can only be applied to linear systems, and some nonlinear anti-windup control methods for nonlinear systems require much online calculations to obtain the control law, which is not conducive to real-time control. Therefore, a novel control method was applied to the nonlinear research object. The nested saturation function could realize the bounded amplitude and differential of the input when used as a control law because of its specific form. Thus, it could be used to solve the amplitude and rate saturation problems in an aerostat system. This paper presented the design of an anti-windup controller for a nonlinear multi-propeller aerostat with amplitude and rate saturations of control input. First, the three-DOF model of the aerostat was established and transformed into two chain-like integral systems by taking forces other than propeller thrust as disturbances. Based on the theory of nested saturation control, the relationship between the amplitude and rate saturations of control inputs and the parameters of saturation function was obtained. Taking the aerostat as the research object, decoupled controller for longitudinal and lateral channels was designed to realize the bounded amplitude and rate of the system input. The global stability of the system was proved by the Lyapunov stability theorem, and the dynamic performance of the system was analyzed under different adjustable parameters. Considering the wind disturbance, the effectiveness and robustness of the controller was verified by simulations. 
Keywords:
本文献已被 万方数据 等数据库收录!
点击此处可从《》浏览原始摘要信息
点击此处可从《》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司    京ICP备09084417号-23

京公网安备 11010802026262号