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 is the first time that ignition motor which successful used for an air-to-air missile. Which provides a good method for the design of next generation ignition motor.

这是首次成功地应用于空空导弹发动机上的点火发动机，从而为后续空空导弹固体火箭发动机点火装置的设计提供了一条新的途径。

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。