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一体化制导综合控制平台的研究

黑蕾 陈肖雨 王江

兵工自动化2025,Vol.44Issue(1):1-4,14,5.
兵工自动化2025,Vol.44Issue(1):1-4,14,5.DOI:10.7690/bgzdh.2025.01.001

一体化制导综合控制平台的研究

Research on Integrated Guidance and Control Platform

黑蕾 1陈肖雨 1王江1

作者信息

  • 1. 中国航天科技集团公司第四研究院第四十一研究所 115 室,西安 710025
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摘要

Abstract

In order to meet the requirements of high integration,high performance and low cost of the core components on the missile,a new type of flight control and guidance integrated platform on the missile is designed by using the integrated design concept of comprehensive processing,which integrates the functions of multiple components on the missile,simplifies the system architecture,and has passed many flight tests.The test results show that the platform has stable performance,compact structure,high reliability and high control precision,and meets the design requirements of missile control system.

关键词

一体化/制导组合/弹上部件

Key words

integration/guidance combination/missile-borne components

分类

军事科技

引用本文复制引用

黑蕾,陈肖雨,王江..一体化制导综合控制平台的研究[J].兵工自动化,2025,44(1):1-4,14,5.

兵工自动化

OA北大核心

1006-1576

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