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[an error occurred while processing this directive]舰空导弹拦截目标中制导律设计研究
The Design Research on the Midcourse Guidance Law of Ship-to-air Missile
Received date: 2017-07-04
Online published: 2025-05-30
孙旭涛 , 郭小威 , 王志佳 . 舰空导弹拦截目标中制导律设计研究[J]. 弹箭与制导学报, 2018 , 38(3) : 29 -32 . DOI: 10.15892/j.cnki.djzdxb.2018.03.007
In order to reduce the target interception time and avoid complex iterative computation of the general guidance law, we designed a variable coefficient target interception midcourse guidance law on the basis of prediction hit according to three dimension guidance law, prediction hit and other guidance laws. Simulation results improved that the target interception guidance law is a practical guidance law which has less time to intercept target and better response to ship-to-air missile speed.
Key words: ship-to-air missile; midcourse guidance law; predict hit
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