本文提出了一套完整的变后掠飞机在变后掠过程中从气动力直至航迹计算的数值求解方法。

A numerical method to obtain a complete solution of the dynamic response of a variable sweep wing aircraft in the course of changing the angle of sweep is presented in this paper.

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提出一种计算航迹纯度的方法，解决了融合航迹与目标真实轨迹的关联这一关键技术难题。

In this paper, a method for calculating track purity is proposed in order to realize the correlation between fusion tracks and true target tracks.

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计算结果表明，所采用的控制律可以实现运载器跟随拖曳飞机的飞行航迹。

The simulating results indicate that these flight path control laws can ensure the vehicle flies following the flight track of the towing plane.

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