| 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.[点击复制] |
| ZHOU Jun and ZHOU Fengqi.Physical Simulation Experiment Analysis forVariable Structure Control Systems of Flexible Satellites[J].Control Theory and Technology,1998,15(4):583~588.[点击复制] |
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| 挠性卫星变结构控制的全物理仿真实验分析* |
| Physical Simulation Experiment Analysis forVariable Structure Control Systems of Flexible Satellites |
| 摘要点击 821 全文点击 379 投稿时间：1996-08-26 修订日期：1997-05-04 |
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| DOI编号 |
| 1998,15(4):583-588 |
| 中文关键词 挠性结构 变结构控制 全物理仿真实验 |
| 英文关键词 flexible structure variable structure control physical simulation experiment |
| 基金项目 |
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| 中文摘要 |
| 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. |
| 英文摘要 |
| 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. |