A full-band antenna array and radome integrated simulation method
A simulation method and radome technology, which are applied in special data processing applications, instruments, electrical digital data processing, etc., can solve the problem that the accuracy and speed requirements cannot be met at the same time, and the RWG moment method is difficult to effectively solve the electrical large-scale, complex-shaped objects. Problems such as the inability to obtain accurate results in the calculation
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Embodiment 1
[0086] figure 1 It is a flow chart of an integrated simulation method for a full-band antenna array and a radome in a preferred embodiment of the present invention.
[0087] Such as figure 1 As shown, this embodiment provides a full-band antenna array and radome integrated simulation method, including at least:
[0088]Step S1: The simulation platform calls the geometric model module, reads the imported geometric graphics file, extracts geometric feature data, and establishes the geometric model of the antenna and radome.
[0089] Specifically, the geometric model module includes: a geometric feature data import module, which is used to realize the unified reading of geometric graphic files in different formats; a geometric feature modeling module, which extracts the geometric feature data of the imported geometric graphic files, and establishes a geometric model ; The geometric feature data export module is used to export geometric model data files. The format of the impor...
Embodiment 2
[0165] This embodiment provides a simulation platform for integrated simulation of full-band antenna array and radome, including a pre-processing module, an algorithm solving module and a post-processing module.
[0166] 1) Pre-processing module
[0167] The pre-processing module is mainly used to import a variety of aircraft models, directly support STL, IGES, STEP and other 3D models, support surface repair and optimization functions, and directly import material libraries.
[0168] Specifically, this module supports the geometric model of the full-detailed aircraft without simplification; it is convenient to set parameters such as initial frequency, boundary conditions, and excitation field sources; the calculation grid adaptive parameter definition; the material library can be directly imported into the model to be parameterized and Script control, convenient for design and optimization; support import of various aircraft and antenna models; support surface repair optimiza...
Embodiment 3
[0176] Simulation example: simulation analysis of radome antenna radiation characteristics
[0177] In this embodiment, algorithm verification is carried out by means of experimental measurement. In this example,
[0178] 1) Using the high-order moment method to quickly simulate the far-field radiation characteristics of the radome antenna;
[0179] 2) The diameter of the feedforward reflector is 9m, the diameter of the radome is 12.8m, and the simulation frequency band is 2.7-2.9GHz;
[0180] 3) Simulation time: 3 minutes without cover, 1.5 hours with cover.
[0181] Figure 4 A comparison chart of transmittance at different frequencies is given.
[0182] Such as Figure 4 As shown, curve A represents a single antenna, curve B represents an antenna plus a reflector, and curve C represents an antenna plus a reflector plus a radome. Wherein, the abscissa represents frequency (GHz), and the ordinate represents return loss (dB).
[0183] Depend on Figure 4 It can be seen...
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