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The influence of the navigation direction of the dual stealth aircraft formation on the performance of monopulse radar

机译:双隐身飞机编队导航方向对单脉冲雷达性能的影响

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Aiming at the problem of how to effectively compare and analyze the influence of the angle tracking error of monopulse radar caused by the difference of the dual stealth aircraft formation in the formation navigation direction, the dynamic track model of the dual stealth aircraft in different navigation directions is established for the first time, and the acquisition method of the dynamic RCS of the formation under different navigation directions is put forward. Using the time-varying dynamic signal-to-noise ratio of the dual stealth aircraft in different flight directions as parameters, the monopulse radar angle tracking error solving model suitable for the cooperative flight of dual stealth aircraft is established. This paper analyzes the influence of the difference of the dual aircrafts’ heading direction on the angle tracking error performance of monopulse radar. It is the first time to conclude that the angle tracking error of monopulse radar will increase obviously with the increase of the heading angle of dual stealth aircraft when there is no interference.
机译:针对如何有效地比较和分析双隐形飞机编队在编队导航方向上的差异引起的单脉冲雷达角度跟踪误差的影响,提出了双隐形飞机在不同导航方向上的动态跟踪模型。首次建立了航向模型,提出了不同导航方向下地层动态RCS的获取方法。以双隐身飞机在不同飞行方向的时变动态信噪比为参数,建立了适合双隐身飞机协同飞行的单脉冲雷达角跟踪误差求解模型。本文分析了双机航向方向差异对单脉冲雷达角度跟踪误差性能的影响。首次得出结论,在无干扰的情况下,单脉冲雷达的角度跟踪误差会随着双隐身飞机航向角的增加而明显增加。

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