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Journal of Projectiles, Rockets, Missiles and Guidance >

2019 , Vol. 39 >Issue 6: 21 - 24

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2019.06.006

Trajectory Simulation and Performance Evaluation for X-type Guided Rocket Submunition

  • WANG Haifeng ,
  • WANG Guangwei ,
  • JIA Bo ,
  • SHAO Qingxin
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  • 63850 Unit No., Jilin Baicheng 137000, China

Received date: 2018-10-11

  Online published: 2025-05-12

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Abstract

In order to evaluate the trajectory performance of x-type guided rocket submunition, the ballistic model was established, and the precision method of key ballistic parameters was designed, the maximum range assessment under the boundary condition is achieved through accurate trajectory simulation.The method has been applied to the actual model PET and solved the ballistic performance evaluation problem where the altitude of launching position is zero meters.

Key words： guided rocket; trajectory simulation; ballistic performance evaluation

Cite this article

WANG Haifeng , WANG Guangwei , JIA Bo , SHAO Qingxin . Trajectory Simulation and Performance Evaluation for X-type Guided Rocket Submunition[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2019 , 39(6) : 21 -24 . DOI: 10.15892/j.cnki.djzdxb.2019.06.006

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