a missile designed to be launched from one airplane at another

this paper investigates the large angle attitude post stall maneuver control for the agile turn phase of an air-to-air missile that has high off-boresight capability and head reverse maneuverability.

为研究具有大离轴角及越肩发射能力的先进空空导弹初始段敏捷转弯方法，研究了装有反作用喷气控制系统的空空导弹的大角度姿态过失速机动控制律。

on the basis of missile six degrees of freedom equation of state, we used the non-linearity dynamic inversion methods to design air-to-air missile basic control law;

首先在推导出导弹六自由度状态方程的基础上采用非线性动态逆方法设计空空导弹的基本控制律；

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。

the rapid development of tactical air-to-air missile puts forward a variety of new requirements and challenge to radome, and constantly drives it to seek new ways to technique breakthrough.

战术空空导弹的迅速发展，对作为其重要部件的导弹天线罩提出了一系列新的需求和挑战，同时，也带动了导弹天线罩不断地寻求新的技术途径和突破。

this paper , in connection with ir target signature research, deals with the principle and realization for the ir imaging terminal-guidance technology of air-to-air missile in clutter background.

通过结合目标红外特征，研究了空-空弹在复杂背景条件下的目标红外成像末制导的技术原理和实施途径。

then, the storage phase, standby phase, captive flight phase and free flight phase of the typical life profile of air-to-air missile are emphatically expounded.

之后对空空导弹典型寿命剖面中的贮存阶段、待命阶段、挂飞阶段、自主飞行阶段进行了重点阐述。

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。

in the newscast, the way a target was hit by the air-to-air missile fired by a j-10 fighter aircraft and exploded looks almost identical to a cinema scene from the hollywood film top gun.

新闻画面中，靶机被歼十战机发射的空空导弹击中并爆炸的场面和好莱坞影片《壮志凌云》中的镜头简直一模一样。

an adaptive robust controller with l_2-gain performance has been designed for roll-movement of air-to-air missile with thrust vector.

针对推力矢量空空弹横滚运动的模型，设计了基于性能準则的自适应控制器。

firstly, the basic composition of air-to-air missile image guidance system is provided. secondly, we propose the principle of operation and realizing method of image guidance equipment.

首先以某原準弹为基础，探讨了空空导弹成象制导系统的组成原理，然后给出了成象制导设备的工作原理和实现方法。

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。

the paper analyses the importance of measuring vibrating data of air-to-air missile in flying experiment, it introduces a multi-range acquisition method of air-to-air missile vibrating sensor signal.

分析了準确测量空空导弹在飞行试验中振动数据的重要性，介绍了一种空空导弹振动传感器信号多量程采集的方法。