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Journal of Projectiles, Rockets, Missiles and Guidance >

2012 , Vol. 32 >Issue 1: 29 - 32

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.01.032

MISSILES AND GUIDANCE TECHNOLOGY

Dynamic Analysis and Kinematic Simulation for Earth Rotation Effect on Ballistic Missile Range

  • XIA Weiwei ,
  • MU Jianhua ,
  • QU Jishuang ,
  • FU Zhimin
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  • The Second Artillery Equipment Academy, Beijing 100085, China

Received date: 2011-05-05

  Online published: 2025-05-29

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Abstract

For analyzing the effect of earth rotation on missile range, the change rule with different trajectory shape was discussed by a dynamic analysis based on launch coordinate system. The impact point changed from eastward region to westward region with increase of the burnout point slope angel, which was validated by a kinematic simulation based on inertial coordinate system. The conclusion is that launch towards east is beneficial for increasing the range when considering the actual burnout point slope angel scope of the maximum range trajectory.

Key words： ballistic missile; earth rotation; elliptic orbit; missile range

Cite this article

XIA Weiwei , MU Jianhua , QU Jishuang , FU Zhimin . Dynamic Analysis and Kinematic Simulation for Earth Rotation Effect on Ballistic Missile Range[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(1) : 29 -32 . DOI: 10.15892/j.cnki.djzdxb.2012.01.032

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