| 陆基移动小运载制导控制技术初探 |
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| 引用本文： | 高晓颖.陆基移动小运载制导控制技术初探[J].航天控制,2004,22(3):23-25. |
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| 作者姓名： | 高晓颖 |
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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： | 陆基移动发射小型运载器不依赖大型、复杂的地面支持系统 ,系统简单 ,可以根据轨道以及相关限制因素需要选择最佳发射地点与控制程序 ,进而大幅度降低发射成本、有效的提高运载能力。本文根据上述特点 ,基于惯性 /卫星组合技术研究了制导控制方案 ,可以实现行进中瞄准与快速发射 ,并以近地轨道卫星发射为范例进行仿真计算。
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| 关 键 词： | 运载器 制导 控制 |
| 文章编号： | 1006-3242(2004)03-23-03 |
| 修稿时间： | 2003年7月10日 |
Study of Guidance and Control Technology for Land-based Mobile Small Launch Vehicle |
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| Gao Xiaoying Beijing Aerospace Automatic Control Institute,Beijing.Study of Guidance and Control Technology for Land-based Mobile Small Launch Vehicle[J].Aerospace Control,2004,22(3):23-25. |
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| Authors: | Gao Xiaoying Beijing Aerospace Automatic Control Institute Beijing |
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| Institution: | Gao Xiaoying Beijing Aerospace Automatic Control Institute,Beijing 100854 |
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| Abstract: | Land-based mobile launching small launc h ve hicle has some characters, such as simple, independent of large and complex grou nd support system, and it could select the most suitable position and program to meet the need of orbit and other limited conditions, also it has lower cost and higher carry ability. Based on inertial/satellite composite navigation technolo gy and the characters mentioned above, a proposal of guidance and control is dis cussed in this paper. This proposal could take aim in flight and launch quickly. In the end, a simulation computing LEO satellite shooting is gi ven as an example. < |
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| Keywords: | Carrier Guidance Control |
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