| 实时微分控制的算法研究 |
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| 引用本文： | 陈磊,王海丽,任萱.实时微分控制的算法研究[J].航天控制,2001,19(4):48-52. |
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| 作者姓名： | 陈磊 王海丽 任萱 |
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| 作者单位： | 国防科技大学航天与材料工程学院,长沙,410073 |
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| 基金项目： | 国家高技术计划 86 3- 40 9项目资助 |
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| 摘 要： | 实时微分控制是进行航天器轨道控制的主要方法。本文在费景高所提出的算法基础上 ,提出了一种有效的改进算法 ,扩大了算法的适用范围。文章对算法的稳定性进行了研究 ,并给出了此算法在弹道导弹显式制导中的应用实例。
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| 关 键 词： | 轨道控制 算法 制导 |
| 修稿时间： | 2001年4月25日 |
The Research of Real- Time Differential Control Algorithm |
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| Chen Lei\ Wang Haili\ Ren Xuan College of Aerospace and Material Engineering,National University of Defense Technology,Changsha.The Research of Real- Time Differential Control Algorithm[J].Aerospace Control,2001,19(4):48-52. |
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| Authors: | Chen Lei\ Wang Haili\ Ren Xuan College of Aerospace and Material Engineering National University of Defense Technology Changsha |
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| Institution: | Chen Lei\ Wang Haili\ Ren Xuan College of Aerospace and Material Engineering,National University of Defense Technology,Changsha 410073 |
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| Abstract: | Real-time differential control is a major method to control the trajectory of spacecraft. An efficient algorithm is presented based on the algorithm presented by Fei Jinggao. The new algorithm can be used in more instances than the old one. The stability of the new algorithm is discussed in the paper.The algorithm is used in the guidance of ballistic missile in the end. |
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| Keywords: | Orbital control\ Algorithm\ Guidance |
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