引用本文:刘骏,王晓光,王宇奇,林麒.风洞试验绳牵引并联支撑系统自适应滑模控制[J].控制理论与应用,2019,36(9):1477~1485.[点击复制]
LIU JUN,WANG Xiao-guang,WANG Yu-qi,LIN Qi.Adaptive sliding mode control of wire-driven parallel suspension system in wind tunnel tests[J].Control Theory and Technology,2019,36(9):1477~1485.[点击复制]
风洞试验绳牵引并联支撑系统自适应滑模控制
Adaptive sliding mode control of wire-driven parallel suspension system in wind tunnel tests
摘要点击 1746  全文点击 679  投稿时间：2018-03-02  修订日期：2019-05-24
查看全文  查看/发表评论  下载PDF阅读器
DOI编号  10.7641/CTA.2019.80135
  2019,36(9):1477-1485
中文关键词  风洞试验  绳牵引并联支撑  自适应  滑模控制  奇异摄动  
英文关键词  Wind tunnel tests  Wire-driven parallel suspension  Adaptive  Sliding mode control  Singular perturbation
基金项目  省自然科学基金,国家自然科学基金
作者单位E-mail
刘骏 厦门大学航空航天学院 454600560@qq.com 
王晓光* 厦门大学航空航天学院 xgwang@xmu.edu.cn 
王宇奇 厦门大学航空航天学院  
林麒 厦门大学航空航天学院  
中文摘要
      针对绳牵引并联支撑系统在风洞试验中的应用，提出一种自适应滑模控制方法以提高飞行器模型动态试验的运动精度。首先，详细分析了系统不确定因素，并重点考虑了气动力与绳弹性变形的影响，重构了系统动力学方程；基于奇异摄动理论，提出一种复合控制律，其中对慢变状态量采用自适应连续非奇异终端滑模控制，对快变状态量采用微分控制；通过李雅普诺夫函数法对系统的稳定性进行了分析，确定了控制律中微分增益项的影响。最后，以两种典型的动态轨迹为例，考虑气动力建模，对所设计控制律进行多参数仿真分析。结果表明该复合控制律可以减小绳弹性以及气动力等不确定性参数对跟踪误差的影响，提高运动控制精度，因此该控制方法有效可行，可为绳牵引并联支撑的动态试验应用提供理论指导。
英文摘要
      Adaptive sliding mode control method is proposed to achieve high precision motion of aircraft model, which is suspended by wire-driven parallel robot in wind tunnel tests. Firstly, uncertainties in system parameters are analyzed in detail, and the aerodynamic forces and wire elastic properties are especially considered in the reconstruction of system dynamic equations. Secondly, a composite control law is designed based on the singular perturbation theory, in which slow variables are dealt with adaptive continuous non-singular sliding mode control, and fast variables are coped with differential control. Then, stability of the overall closed-loop system is analyzed through Lyapunov function method, and differential gains in the control law are determined. Finally, two typical dynamic test trajectories for aircraft model are taken as examples. Taking aerodynamic forces into account, numerical simulation is conducted by using this compound control law. Simulation results show that the tracking error induced by parameters uncertainties and elastic properties could be decreased by the proposed control method, and it’s quite effective and feasible, which could provide theoretical guidance for the wire-driven parallel suspension system in dynamic wind tunnel tests.