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BALLISTIC AND AIRDYNAMICS

The Equation and Simulation for Unpowered Trajectory of Ballistic Missiles

  • HU Chuanjun ,
  • YANG Huixian
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  • Faculty of Material, Optoelectronics and Physics, Xiangtan University, Hunan Xiangtan 411105, China

Received date: 2009-07-27

  Online published: 2025-05-28

Abstract

In unpowered trajectory of ballistic missiles, according to the role of air drag from its trajectory can be divided into free-flight trajectory and reentry trajectory in two parts. The paragraph [1] is simulation analysis for free-flight trajectory and the paragraph [2] is simulation analysis for reentry trajectory. In fact, the free-flight trajectory and reentry trajectory has close contacts, through these contacts, established unpowered trajectory of ballistic missiles applying to the entire trajectory equations. Finally, as an example of a certain model of short-range ballistic missiles to carry out the establishment of a simulation model, through simulation and analysis of results, the model can be a better reflection of the dynamic characteristics of ballistic missiles' unpowered trajectory.

Cite this article

HU Chuanjun , YANG Huixian . The Equation and Simulation for Unpowered Trajectory of Ballistic Missiles[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(4) : 131 -133 . DOI: 10.15892/j.cnki.djzdxb.2010.04.053

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Outlines

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