本论文主要是研究卡尔曼滤波参数混合技术应用于民用飞机相对导航系统。

This paper discusses mainly the technique of parameter hybrid of Kalman filter applied in the system of relative navigation.

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机械学工程将这些原理应用于现实生活来处理核反应堆，混合动力汽车，实验性飞机，导弹导航系统等各种问题。

Engineering mechanics applies these principles to real-world design problems as diverse as nuclear reactors, hybrid automobiles, experimental aircraft, and missile guidance systems.

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