| 航天器轨道控制系统的智能设计方法与仿真 |
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| 引用本文： | 徐肖豪,刘淑祥.航天器轨道控制系统的智能设计方法与仿真[J].航天控制,1993(2). |
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| 作者姓名： | 徐肖豪 刘淑祥 |
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| 作者单位： | 南京航空学院自动控制系，南京航空学院自动控制系 |
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| 基金项目： | 国家自然科学基金资助的项目 |
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| 摘 要： | 本文介绍了将智能控制方法用于航天器交会对接段的轨道控制。通过建立系统的特征模型、知识库、数据库和规则库并且构造出相应的推理机构和控制逻辑,为航天器的轨道控制过程设计了一种专家式智能控制器。仿真结果表明了此系统具有较好的跟踪性能。
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| 关 键 词： | 智能控制 轨道控制 会后 对接 |
The Design and Simulation of Intelligent Controller for Spacecraft Orbil Control System |
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| Xu Xiaohao Liu Shuxiang Nanjing Aeronautical Institude.The Design and Simulation of Intelligent Controller for Spacecraft Orbil Control System[J].Aerospace Control,1993(2). |
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| Authors: | Xu Xiaohao Liu Shuxiang Nanjing Aeronautical Institude |
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| Institution: | Xu Xiaohao Liu Shuxiang Nanjing Aeronautical Institude,Department of Automatic Control |
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| Abstract: | The method of intelligent control applied to the orbital control of rendezvous and docking phase of spacecraft is presented in this paper. By establishing the characteristic model, the knowledge base, the data base and the rule base of systems and constructing the ijference mechanism and control strategy, an expert intelligent controller for the orbital control is designed. The digital simulation displays that this system has good control performance and strong adaptability. |
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| Keywords: | Intelligent contro Orbital control Rendezvous Docking |
| 本文献已被 CNKI 等数据库收录！ |
