In this paper, one advanced air-to-air missile system has been analyzed in order to determine the main characteristics which are sensitive to the boundary of the allowable launch envelope. An algorithm of allowable launch envelope is derived from this analysis. 本文首先分析了一种先进的空空导弹系统(AAMS),确定导弹对允许发射区边界敏感的主要性能特点,在此基础上提出了导弹允许发射区的算法。
Research on Integrated Logistics Support for Air-to-Air Missile System(AAMS) 空空导弹系统(AAMS)综合保障工作探讨
Test and Analysis of Information Transmit Delay in Air-to-Air Missile System(AAMS) 空空导弹系统(AAMS)信息延迟时间的测试及分析
Based on the mathematical model of air-to-air missile control system, a variable structure control law is designed. 对空空导弹控制系统建立了数学模型,并在此基础上设计了变结构控制律。
Study of Variable Structure Control for the Air-to-Air Missile Control System 变结构控制在空空导弹控制系统中的应用研究