介绍了正交试验设计的基本方法,并应用此方法对反弹道导弹目标打靶试验进行了设计。
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针对强敌空袭目标常以编队的形式实施空袭这一特点,运用排队论理论和概率论知识尝试解决防空导弹体系拦截空中目标群效能问题。
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Pyongyang also says it will use force against any outside opposition to the missile launches.
平壤还说,北韩会使用武力来对付针对导弹试射的任何外部反对.
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从构型和控制律设计两方面入手研究该类导弹跟踪控制问题。
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Application of Quantitative Feedback Theory to Attack Angle Robust Control System of Missile
数量反馈理论在导弹攻角鲁棒控制系统中的应用
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The Design for Autopilot of Large Attack Angle Missile by Using Feedback Linearization Method
大攻角飞行导弹自动驾驶仪反馈线性化设计
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Nonlinear State Feedback Control of Pitch Motion for Reentry Missile with a Large Attack Angle
再入弹头大攻角俯仰运动的非线性状态反馈控制
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Its object is to design the pitch program for a missile by giving attack angle program.
其目的是根据给定导弹的攻角方案设计其俯仰角方案。
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New advance of EO missile approximating warning system abroad is briefly described in this paper.
综述国外导弹逼近红外告警和紫外告警系统的最新进展.
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Analysis and Study on the Reliability Requirement of Antitank Missile Weapon System
反坦克导弹武器系统可靠性要求分析与研究
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Evaluation Method of Flight Training Quality of Antitank Missile Training Simulator
反坦克导弹飞行模拟训练成绩评定方法
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本文介绍了在虚拟环境中,攻顶反坦克导弹实时仿真系统的总体设计。
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Design Method of Flying over Guidance System of Antitank Missile with Strapdown TV Guidance
捷联电视制导反坦克导弹掠飞制导系统设计方法
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The Signature of Anti-Ballistic Missile Treaty and the Withdrawal of the United States
《限制反弹道导弹系统条约》的签订与美国的退出
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