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挠性卫星变结构控制的全物理仿真实验分析*
引用本文:周 军,周凤岐.挠性卫星变结构控制的全物理仿真实验分析*[J].控制理论与应用,1998,15(4):583-588.
作者姓名:周 军  周凤岐
作者单位:西北工业大学航天工程学院!西安,710072
摘    要:我国首次挠性卫星振动控制的全物理仿真实验是基于变结构控制方案完成的。本文针对这一实验着重分析了在控制受限情况下其变结构控制系统镇定无限维挠性结构的稳定性、控制方案与系统喷气或燃料消耗的关系等问题,取得了具有实际意义的结论。

关 键 词:变结构控制  全物理仿真实验  卫星  姿态控制  挠性
收稿时间:1996/8/26 0:00:00
修稿时间:5/4/1997 12:00:00 AM

Physical Simulation Experiment Analysis forVariable Structure Control Systems of Flexible Satellites
ZHOU Jun,and,ZHOU Fengqi.Physical Simulation Experiment Analysis forVariable Structure Control Systems of Flexible Satellites[J].Control Theory & Applications,1998,15(4):583-588.
Authors:ZHOU Jun  and  ZHOU Fengqi
Abstract:In this paper, two problems are analysed to the physical simulation experiments of flexible satellite vibration active suppression,which are successfully done for the first time in our country. The first is the stability problem of flexible structures' bounded variable structure active control systems,the second is the relations between the control scheme and the gas or fuel consumption that a control system needs. Many important conlusions with practical significance are got.
Keywords:flexible structure  variable structure control  physical simulation experiment
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