Research on Multi-Stage Overall Parameter Optimization Method for Boost-glide Missile

LUO Wei; LEI Gang; ZHENG Xiaolong

doi:10.15892/j.cnki.djzdxb.2023.05.012

Journal of Projectiles, Rockets, Missiles and Guidance >

2023 , Vol. 43 >Issue 5: 73 - 79

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2023.05.012

Research on Multi-Stage Overall Parameter Optimization Method for Boost-glide Missile

LUO Wei ,
LEI Gang ,
ZHENG Xiaolong

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Rock Force University of Engineering,Xi’an 710025,Shaanxi, China

Received date: 2022-10-26

Online published: 2024-12-30

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Abstract

In order to give full play to the maximum combat effectiveness of the booster-glide missile, its overall parameters are optimized under certain flight conditions. Firstly, after analyzing the influence of various parameters on the flight trajectory under the direct takeoff and gliding trajectory, the entire optimization process is divided into two relatively independent sub-stages; then the sub-stages are optimized by adaptive genetic algorithm respectively, and the results satisfying each The optimal missile overall design scheme under the class constraints; finally, the method is verified based on the Monka simulation. The results show that the design method can complete the overall parameter optimization within 5.5 seconds, and make the missile fly with the accuracy of ±0.7%.

Key words： booster-glide missile; overall parameter design; segmentation optimization method; adaptive genetic algorithm

Cite this article

LUO Wei , LEI Gang , ZHENG Xiaolong . Research on Multi-Stage Overall Parameter Optimization Method for Boost-glide Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2023 , 43(5) : 73 -79 . DOI: 10.15892/j.cnki.djzdxb.2023.05.012

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