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基于趋近律滑模控制的气浮十字梁实验系统复合控制研究
引用本文:邹荣平,支岳,邱立军.基于趋近律滑模控制的气浮十字梁实验系统复合控制研究[J].海军航空工程学院学报,2008,23(4):371-374, 379.
作者姓名:邹荣平  支岳  邱立军
作者单位:海军驻天津地区航空军事代表室,天津,300140;海军航空工程学院,研究生管理大队,山东,烟台,264001;海军航空工程学院,科研部,山东,烟台,264001
摘    要:文章推导了具有双执行机构的十字梁实验系统三自由度运动动力学方程,设计了一个基于趋近律的滑模变结构控制器,对纵向运动模型进行了数学仿真,为深入探讨气动-质量矩复合控制奠定了基础。

关 键 词:复合控制  共栖  十字梁  趋近律

Research on The Composite Control Over Gas-flotage Cross Beam Experiment System Based on Reaching Law Sliding Mode Control
ZOU Rong-ping,ZHI Yue and QIU Li-jun.Research on The Composite Control Over Gas-flotage Cross Beam Experiment System Based on Reaching Law Sliding Mode Control[J].Journal of Naval Aeronautical Engineering Institute,2008,23(4):371-374, 379.
Authors:ZOU Rong-ping  ZHI Yue and QIU Li-jun
Institution:ZOU Rong-ping, ZHI Yue, QIU Li-jun ( 1. Aeronautical Military Representatives Office of Navy in Tianjin, Tianjin 300140, China; 2. Naval Aeronautical and Astronautical University a. Graduate Students' Brigade; b. Department of Scientific Research, Yantai Shandong 264001, China)
Abstract:The three degrees of freedom dynamic equation of gas-flotage crossbeam with double operators based on composite control of aerodynamics-mass moment was derived. A sliding mode variable structure controller based on reaching law was designed in this paper. Simulation and practicality experiment about the crossbeam attitude confined to vertical plane was performed, which laid a foundation on developing the composite control of aerodynamics-mass moment control.
Keywords:composite control  commensalisms phenomenon  crossbeam  reaching law  
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