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.
本文首先分析了一种先进的空空导弹系统，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。
Introduces the calibration technique of fuze shielding transmit-receive isolation, forward transmission and the test method of fuze initiation property in the air to air missile system test.
介绍了空空导弹总体试验中引信屏蔽罩收发隔离度、正向传输插损的标定技术和引信启动特性测试方法。
A mini digital Attitude and Heading Reference System (AHRS) based on DSP is designed, which can be used on air-to-air missile with Strapdown Inertial Navigation System (SINS) as mid-course guidance.
论文针对使用捷联惯导系统为中制导的近距空空导弹，设计了一种基于数字信号处理器(dsp)的小型数字式捷联航姿应用系统。
With the complexity of the air attack environment, US pay more attention to develop the integrated operation of US air and missile defense system.
随着现代空袭环境的日益复杂化，美国更加注重防空反导系统一体化作战能力的建设。
This method are with a high accuracy and real time application, and can be applied in the calculation of allowable launching area of air to air missile in air borne fire control system.
提出了一种确定目标进入角的原理和方法，这种原理和方法具有较高的计算精度和实时性，易于工程实现，可用于机载火力控制系统完成空对空导弹允许发射区计算。
The stability analysis of variable structure guidance system of an air-to-air missile was conducted based on the circle criterion nonlinear stability analysis theory.
文中在圆判据非线性稳定性理论基础上，进行空空导弹变结构制导系统的稳定性分析。
This paper analyzes the weakness of ground (ship) to air missile systems with CW guidance system to attack low speed targets (such as helicopters) and static air targets (balloon targets).
分析了连续波制导体系的地(舰)空导弹武器系统难以攻击低速目标(武装直升机)和空中静目标(气球靶)的弱点，并从原理上进行了分析。
In fact, the reason the U. S. air Force chose the air-launched anti-satellite system is that it does not have to have its target line up with a ground-based missile pad.
事实上这也是美国选择空基反卫星武器的原因：目标卫星轨道不需要被改变。
The important role of the long range air defense missile in the air defense system is emphasized. The long range air defense missile's tasks and the major method to achieve the goal are discussed.
强调了远程防空导弹在防空体系的地位，讨论了远程防空导弹作战使命及主要技术途径的实现思想。
Availability, dependability and system availability of the double-passage air-to-air middle-far-distance missile weapon system are analyzed. And the efficiency count formulas are given.
分析并给出了双通道空空中远程导弹武器系统的可用性、可信性、系统能力和效能计算公式。
Availability, dependability and system availability of the double-passage air-to-air middle-far-distance missile weapon system are analyzed. And the efficiency count formulas are given.
分析并给出了双通道空空中远程导弹武器系统的可用性、可信性、系统能力和效能计算公式。
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