导弹与制导技术

几种增大空地导弹落角的制导方式比较

  • 明宝印 ,
  • 高士英 ,
  • 邢强 ,
  • 丁庆海 ,
  • 罗振宇
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  • 1 空军装备研究院装备总体论证研究所,北京 100076
    2 北京航空航天大学宇航学院,北京 100083

明宝印(1975-),男,河南信阳人,工程师,研究方向:机载导弹总体技术和导航、制导与控制。

收稿日期: 2011-02-21

  网络出版日期: 2025-05-30

Comparison of Some Guidance Modes for Widening the Impact Angle of Air-to-ground Missile

  • MING Baoyin ,
  • GAO Shiying ,
  • XING Qiang ,
  • DING Qinghai ,
  • LUO Zhenyu
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  • 1 Research Institute on General Development and Evaluation of Equipment, AFEA, Beijing 100076, China
    2 School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

Received date: 2011-02-21

  Online published: 2025-05-30

摘要

为提高对加固掩体、地下指挥控制中心等硬目标的毁伤效果,新型空地导弹需要使用较大的落角攻击目标。文中首先对两种可实现大落角攻击的制导方式——————过重补比例导引和Zarchan弹道成型制导律进行了仿真分析,并提出了“Zarchan弹道+比例导引”组合制导方式,仿真分析表明,该组合制导方式可实现接近90°的末端落角,比较适合于防区外发射空地导弹和高空投放的制导炸弹。

本文引用格式

明宝印 , 高士英 , 邢强 , 丁庆海 , 罗振宇 . 几种增大空地导弹落角的制导方式比较[J]. 弹箭与制导学报, 2011 , 31(6) : 41 -43,50 . DOI: 10.15892/j.cnki.djzdxb.2011.06.039

Abstract

To achieve better lethality for attacking hard targets such as strongly reinforced bunkers, and underground command and control centers, many state-of-the-art air-to-ground missiles need higher impact angles. Over-compensated proportional navigation and trajectory shaping guidance proposed by Zarchan were analyzed and simulated. A new guidance law that combines the method of Zarchan's trajectory shaping guidance and proportional navigation was proposed and studied. The simulations indicate that it can get nearly 90°impact angles, and it is very suitable for standoff air-to-ground missile and guided bombs released from high altitude.

参考文献

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Paul Zarchan. Tactical and strategic missile guidance[M]. 4th ed. Washington: American Institute of Aeronautics and As-tronautics, Inc., 2002.
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