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论文:2013,Vol:31,Issue(2):239-243 |
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引用本文： |
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葛致磊, 李宪强, 郭锐. 弹道导弹主动段拦截导引律研究[J]. 西北工业大学 |
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Ge Zhilei, Li Xianqiang, Guo Rui. Guidance Laws for Boost-Phase Interception of Ballistic Missile[J]. Northwestern polytechnical university |
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| 弹道导弹主动段拦截导引律研究 |
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| 葛致磊, 李宪强, 郭锐 |
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| 西北工业大学 精确制导与控制研究所, 陕西 西安 710072 |
| 摘要: |
| 处于主动段的弹道导弹具有很大的纵向加速度,常规的制导律很容易因为提供的爬升能力不足,使拦截弹在拦截末端陷入尾追,而导致拦截失败,对此,文章分别设计了能够克服目标纵向加速度的中制导律和末制导律。在中制导律的设计中,首先采用了对基于零脱靶量的中制导律引入目标运动补偿项的方法,设计了一种中制导律,此外结合空基反导的特点,通过控制弹目相对高度差和相对偏航距离为零达到控制视线角速度的方法,设计了另一种中制导律。末制导律采用了滑模制导律,仿真结果表明文中所设计的制导律能够以很高的精度拦截目标。 |
| 关键词:
主动段拦截
导引律
空基反导
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| Guidance Laws for Boost-Phase Interception of Ballistic Missile |
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| Ge Zhilei, Li Xianqiang, Guo Rui |
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| Institute of Precision Guidance and Control,Northwestern Polytechnical University. Xi'an 710072,China |
| Abstract: |
| Ballistic missiles in the boost phase have very high longitudinal acceleration. Because of the lack ofclimbing capacity,the conventional guidance law is prone to making the interceptor fall into chase after the target,which will lead to the failure to intercept the target. For that,we design the mid-guidance and homing guidancelaws which can suppress the longitudinal acceleration of the target. Section 1 of the full paper gives the mathemati-cal models respectively of the interceptor and the target. Subsections 2. 1 and 2. 2 design the first kind of mid-guid-ance law; section 2. 3 designs the second kind of mid-guidance law. Section 3 designs the terminal guidance lawwith sliding mode control. The simulation results and their analysis show preliminarily that the guidance laws de-signed can achieve intercepting targets in the boost phase with high precision. |
| Key words:
acceleration
ballistic missiles
computer simulation
design
mathematical models
sliding modecontrol
targets;air-based missile
air-based missile design
boost-phase interception
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| 收稿日期: 2012-05-03
修回日期:
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| DOI: |
| 基金项目: 航天科技创新基金;西北工业大学基础研究基金(JC20100222)资助 |
| 通讯作者:
Email： |
| 作者简介: 葛致磊(1979-),西北工业大学副教授、博士,主要从事导弹精确制导与控制研究。
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| 作者相关文章 |
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| 葛致磊 在本刊中的所有文章 |
| 李宪强 在本刊中的所有文章 |
| 郭锐 在本刊中的所有文章 |
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参考文献: |
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[1] 王 森,杨建军. 战术弹道导弹助推段拦截方法研究. 飞航导弹, 2009, 5: 54-57Wang Sen,Yang Jianjun. Research of Tactical Ballistic Missile Interception Method. Winged Missiles Journal, 2009, 5: 54-57(in Chinese)
[2] 毕世龙,高 倩. 国外机载助推段拦截导弹研制动态. 飞航导弹, 1994, 11: 6-9Bi Shilong,Gao Qian. Development Dynamic of Foreign Airborne Boost Phase Interceptor. Winged Missiles Journal, 1994, 11:6-9 (in Chinese)
[3] 齐艳丽. 美国导弹防御系统动能拦截弹研制与部署现状. 中国航天, 2009, 1: 31-36Qi Yanli. The Development and Deployment Status Quo of U. S. Energy Kinetic Interceptor. Aerospace China, 2009, 1: 31-36(in Chinese)
[4] Jang Sangkeun,Robert G Hutchins,Phillip E Pace. Boost Phase ICBM Engagement Using Space-Based Interceptors: A Com-parison of Guidance Laws. IEEE International Conference on System of System Engineering, 2008, 1-5
[5] Guelman M. Minimum Energy Guidance for Boost Phase Ballistic Missile Interception. Proceedings of the American ControlConference, 1995, 4131-4135
[6] Eric L C,J Brent Romine,Dieter Willner. Boost-Phase Acceleration Estimation. IEEE International Radar Conference, 2000,21-214
[7] 郭 庆,杨 明,王子才. 动能拦截器助推段导引方案研究. 航空动力学报, 2007, 22(2): 310-315Guo Qing,Yang Ming,Wang Zicai. Research on Kinetic Kill Vehicle's Guidance Method in Boost Phase. Journal of AerospacePower, 2007, 22(2):310-315 (in Chinese)
[8] 秦文佳. 弹道导弹助推段攻防效能的仿真分析: [硕士学位论文]. 合肥: 国防科技大学, 2006Qin Wenjia. Simulation and Analysis for Attack-Defense Measures of Ballistic Missile during Boost Phase. Master Degree Dis-sertation,Hefei: Natinal University of Defense Technology, 2006 (in Chinese)
[9] Rakdham B,Tummala M,Pace P E,Michael J B,Pace Z P. Boost Phase Ballistic Missile Defense Using Multiple HypothesisTracking. IEEE International Conference on System of System Engineering, 2007, 1-6
[10] Jennifer C Davis,James J Lisowski. Developing a Remote Staring Sensor for Optimizing Successful Boost Phase Intercept. IEEEAerospace Conference Proceedings, 2002, 4: 1649-1661 |
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