Simulation on Missile-target Intercross Probability of Active Interception Defense System of Helicopter

LI Xue; WEI Jingbiao; LI Yinliang; LI Jianwei

doi:10.15892/j.cnki.djzdxb.2023.04.014

Journal of Projectiles, Rockets, Missiles and Guidance >

2023 , Vol. 43 >Issue 4: 92 - 97

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2023.04.014

Simulation on Missile-target Intercross Probability of Active Interception Defense System of Helicopter

LI Xue ¹ ,
WEI Jingbiao ² ,
LI Yinliang ³ ,
LI Jianwei ³

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¹ Army Aviation School, Beijing 101121,China
² Army Aviation Research Institute, Beijing 101121,China
³ Xi'an Modern Control Technology Research Institute,Xi'an 710065,Shaanxi, China

Received date: 2023-01-09

Online published: 2025-02-07

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Abstract

Aimed at intercross probability of active interception defense system of helicopter in the interception process, the simulation model of intercross was built between interception rocket and incoming ammunition. By means of simulation analysis, influence factor of the system parameter error was computed. The results show that radar ranging error and radar velocity measurement error have no significant influence on intercross probability. Radar angle measurement error, servo rotation error and vertical target dispersion have significant influence on intercross probability. The study can provide guidance to error distribution and parameter analysis optimization of active interception defense system of helicopter.

Key words： helicopter; active interception defense system; intercross probability; simulation

Cite this article

LI Xue , WEI Jingbiao , LI Yinliang , LI Jianwei . Simulation on Missile-target Intercross Probability of Active Interception Defense System of Helicopter[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2023 , 43(4) : 92 -97 . DOI: 10.15892/j.cnki.djzdxb.2023.04.014

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