借鉴导弹导引理论对现代战机的导引机理进行了探讨，推导出一种基于时间最优的飞机导引控制律。
The mechanism of modern fighter guidance is discussed, referring to the theory of missile guidance. A kind of fighter guidance law based on optimal time is given.
分析了弹道终端红外成像导引头跟踪盲区形成的原因，提出了采用局部图像跟踪算法减小跟踪盲区的思想，讨论了飞机目标局部图像跟踪部位的选取原则。
The new infrared imaging fuze realizes forward detection and burst control by sharing the imaging seeker, which can get a series of dynamic infrared images of aircraft from the whole to a part.
末端区域4D导引应首先生成轨迹，然后生成沿该轨迹飞行的高度剖面、合理的速度剖面，最后生成自动引导飞机在规定时间着陆的4D导引指令。
To generate and realize 4D guidance in the terminal area, first there should be ground track , then the altitude profile and appropriate speed profile along the track.
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