| 新一代运载火箭地面测试发控系统一体化设计概述 |
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| 引用本文： | 杜诚谦,潘洁伦.新一代运载火箭地面测试发控系统一体化设计概述[J].航天控制,2004,22(1):55-57. |
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| 作者姓名： | 杜诚谦 潘洁伦 |
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| 作者单位： | 北京航天自动控制研究所,北京,100854 |
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| 摘 要： | 系统介绍了以民用新一代大型运载火箭 (系列 )为背景 ,以一体化设计思想为指导原则 ,开展的地面测试发控系统的研究、设计工作 ,着重论述了以控制系统为核心的一体化设计的必要性和重要性 ,同时对测试发控系统设计方案和总体布局进行了概括阐述。
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| 关 键 词： | 一体化 信息共享 统一供配电 |
| 文章编号： | 1006-3242(2004)01-55-03 |
| 修稿时间： | 2002年7月10日 |
Integrated Design of Ground Test Launch and Control System for New Generation Launch Vehicle |
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| Du chengqian Pan Jielun Beijing Aerospace Automatic Control Institute,Beijing.Integrated Design of Ground Test Launch and Control System for New Generation Launch Vehicle[J].Aerospace Control,2004,22(1):55-57. |
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| Authors: | Du chengqian Pan Jielun Beijing Aerospace Automatic Control Institute Beijing |
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| Institution: | Du chengqian Pan Jielun Beijing Aerospace Automatic Control Institute,Beijing 100854 |
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| Abstract: | Based on large civil launch vehicles and the integrated design theory, the study and design of ground test launch and control system are presented, especially the necessary and feasibility of integrated design for control system, also the general plan and working schedule of ground test launch control system for large launch vehicle are summarized as well. |
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| Keywords: | Integration Information sharing Electric power distribution |
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