| 远程多用途导弹中段制导律 |
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| 引用本文： | 罗喜霜,张天桥. 远程多用途导弹中段制导律[J]. 北京理工大学学报(英文版), 2002, 11(2): 121-124. DOI: 10.3969/j.issn.1004-0579.2002.02.003 |
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| 作者姓名： | 罗喜霜 张天桥 |
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| 作者单位： | 北京理工大学,机电工程学院,北京,100081 |
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| 摘 要： | 提出了一种用于远程多用途导弹的中间段制导律.该制导律分解为两部分,一部分是用在水平导引平面内的制导律,另一部分是铅垂导引平面内的制导律.该中段制导律与末段变结构比例导引律相结合完成整个制导过程.仿真结果表明该中段制导律能满足末段启控条件,使得中、末交班得以顺利完成.
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| 关 键 词： | 多用途导弹 中段制导 起控条件 |
| 收稿时间： | 2001-10-12 |
Mid-Course Guidance Law for Long Range Multi-Purpose Missiles |
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| LUO Xi-shuang and ZHANG Tian qiao. Mid-Course Guidance Law for Long Range Multi-Purpose Missiles[J]. Journal of Beijing Institute of Technology, 2002, 11(2): 121-124. DOI: 10.3969/j.issn.1004-0579.2002.02.003 |
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| Authors: | LUO Xi-shuang and ZHANG Tian qiao |
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| Affiliation: | School of Mechano? Electronics Engineering, Beijing Institute of Technology, Beijing100081, China;School of Mechano? Electronics Engineering, Beijing Institute of Technology, Beijing100081, China |
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| Abstract: | A useful mid course guidance law for long range multi purpose missiles is proposed. The law consists of two parts. One is used in the horizontal guidance plane, and the other in the vertical guidance plane. The mid course is combined with variable structure proportional navigation in the homing phase. Simulation results show that the proposed guidance law can meet the demands for starting up the homing phase and so the handing over between mid course guidance and terminal guidance can be carried out successfully. |
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| Keywords: | multi purpose missile mid course guidance demands for startup |
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