Multi-point thin coating aircraft RCS prediction method with uncertain source
A technology of uncertain sources and prediction methods, applied in the fields of instruments, image data processing, electrical digital data processing, etc., can solve the problems of complex operation, affecting calculation efficiency and accuracy, and complex three-dimensional target shape description, and achieve high computational efficiency. Effect
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[0066] In this embodiment, a typical simulation of the electromagnetic scattering characteristics of a multi-coated aircraft model with an uncertain missile length is carried out. The simulation is performed on a computing platform with an Inter(R)Core(TM)i7-4790K CPU@4.0GHz and a memory of 16GB. Realized above, the coated missile aircraft model such as image 3 As shown, by using the non-rational B-spline surface modeling method, the missile model can be constructed using 53 NURBS patches, and the model shape is controlled by 98 control points, such as Figure 4 shown. The nose of the aircraft is placed along the +z direction, and the median dimensions in the three directions of x, y, and z are 1.37λ×2.6λ×6.3λ respectively, and the change of the projectile length is [-0.5λ,0.5λ] , where λ is the wavelength. In the missile model, the length of the missile body is only determined by Figure 5 The z-direction coordinates of the nine control points are shown. Therefore, it is o...
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