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航天快响发射指挥架构设计与运用OA

Command and control architecture design and application for operationally responsive space launch

中文摘要英文摘要

针对航天快响发射指挥架构设计与运用问题,聚焦典型的 3 级指挥架构和 4 级指挥架构,基于熵理论,采用时效熵和信息熵加权求和的方式构建了指挥架构系统熵模型.研究表明,当时效熵权重 0≤α≤0.6 时,3 级指挥架构更优;当 0.67≤α≤1 时,4 级指挥架构更优;当 0.6<α<0.67 时,则作战分队数量m存在某一阈值u,当m<u时,3级指挥架构更优,当m≥u时,4 级指挥架构更优,且时效熵权重α越大阈值u越小.同时,针对不同的发射方式和不同的产品起始状态,提出了分队耦合运用和精简运用方法.相关模型和方法可为航天快响发射指挥及运用提供参考和理论支撑.

To address the challenge of designing and applying command and control architectures for operationally responsive space launches,the typical three-tier and four-tier architectures are studied.Based on entropy theory,a system entropy mod-el for evaluating these architectures is constructed by integrating weighted timeliness entropy and quality entropy.The find-ings demonstrate that the three-tier architecture is superior when the weight coefficient of timeliness entropy(α)is less than or equal to 0.6,whereas the four-tier architecture proves more effective when α is greater than or equal to 0.67.Within the critical interval of 0.6<α<0.67,a threshold value u for the number of operational units(m)is identified:the three-tier architecture is preferable if m<u,and the four-tier architecture becomes optimal if m≥u.Furthermore,the threshold u decreases as α increases.Corresponding unit employment strategies,namely coupled utilization and streamlined utilization of combat units,are proposed for different launch modes and initial states of the launch vehicle.The models and conclusions can provide a theoretical foundation for decision-making in operationally responsive space launch command and control and its practical application.

毛玺龙;刘星宇;贺绍飞;许兴顺

信息工程大学,河南 郑州 450001||酒泉卫星发射中心,甘肃 酒泉 732750国防科技大学,湖南 长沙 410073酒泉卫星发射中心,甘肃 酒泉 732750酒泉卫星发射中心,甘肃 酒泉 732750

军事科技

航天快响发射指挥架构系统熵分队运用

operationally responsive space launchcommand and control architecturesystem entropyunit application

《指挥控制与仿真》 2026 (2)

1-6,6

10.3969/j.issn.1673-3819.2026.02.001

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