| 防空导弹控制方法的研究现状及展望 |
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| 引用本文： | 吉礼超,宋贵宝.防空导弹控制方法的研究现状及展望[J].战术导弹技术,2009(3):54-59. |
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| 作者姓名： | 吉礼超 宋贵宝 |
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| 作者单位： | [1]海军驻中国航天科技集团公司第七研究院军事代表组,成都610100 [2]海军航空工程学院,烟台264001 |
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| 摘 要： | 系统地论述了用于防空导弹控制的常规和非常规方法的研究现状,分析了它们的特点、适应范围和局限性,并讨论了它们的发展前景.着重论述了直接侧向力控制技术,并指出了实施直接侧向力控制是防空导弹实现精确制导控制的关键,这一技术也必将广泛应用于其它类型的导弹中,成为未来实现高精度制导控制的标志性技术.
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| 关 键 词： | 防空导弹 控制方法 空气动力控制 推力矢量控制 直接侧向力控制 |
Current Study Status and Future Prospect of Control Mode of Air-defense Missile |
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| Affiliation: | Ji Lichao , Song Guibao ( 1. The Working Group on Military of Navy in the Seventh Institute of Aerospace Science And Technology Corporation, Chengdu 610100, China; 2. Naval Aeronautical Engineering Institute, Yantai 264001, China) |
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| Abstract: | Current status of conventional and unconventional control modes of air-defense missile is discussed systematically. Their characteristic, application, shortcoming and prospect are analyzed emphati- cally. Direct lateral force control technology is discussed emphatically. It is pointed out that direct lateral force is a key technology of precise guidance and control of air-defense missile, and the technology will also be applied to other kinds of missile widely, becoming an important technology to realize high precision guidance and control in the future. |
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| Keywords: | air defense missile control mode aerodynamic control thrust vector control direct lateral force control |
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