The Use of Corner Reflectors to Simulate Tactical Aircraft

O. Sukharevsky, I. Ryapolov, V. Vasilets, S. Nechitaylo
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Abstract

Using the methods of mathematical modeling, the values of the radar cross section (RCS) of the Su-27 aircraft model and trihedral corner reflectors in the high-frequency wavelength range were obtained. The scattering characteristics are estimated for trihedral corner reflectors that used as the main scattering element in the proposed model of an airborne radar decoy. The presented results show that in order to obtain sufficiently high values of the RCS of a radar decoy when probing from the front hemisphere, it is necessary to use a “quadruple” corner reflector. If it is necessary to simulate the exact median values of the RCS of a real object in a narrower range of irradiation angles, then it is better to use one tilted corner reflector. It is reasonable to use the obtained results at the developing aerial decoys to simulate the scattering of various complex aerodynamic objects, if corner reflectors are used as a reflective element.
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角反射器在战术飞机模拟中的应用
利用数学建模的方法,得到了苏-27飞机模型和三面角反射器在高频波长范围内的雷达截面(RCS)值。在机载雷达诱饵模型中,以三面角反射器为主要散射元件,对其散射特性进行了估计。研究结果表明,为了在前半球探测时获得足够高的雷达诱饵RCS值,有必要使用“四重”角反射器。如果需要在较窄的照射角度范围内模拟真实物体RCS的精确中值,则最好使用一个倾斜角反射器。如果采用角反射器作为反射元件,将所得结果应用于发展中的空中诱饵来模拟各种复杂气动目标的散射是合理的。
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