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Electric performance-oriented space mesh antenna key dynamical modal selection method

A technology of electrical performance and dynamics, applied in the fields of electrical digital data processing, special data processing applications, instruments, etc.

Active Publication Date: 2017-07-07
XIDIAN UNIV
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  • Description
  • Claims
  • Application Information

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Problems solved by technology

Therefore, aiming at the problem of dynamic key mode selection of spatial mesh antenna, a key dynamic mode selection method oriented to electrical performance is proposed, which overcomes the shortcomings of traditional dynamic mode selection methods and realizes the key dynamic mode selection method in the mode selection process. In the process, the influence of each order mode on the electrical performance of the antenna is fully considered, and the problem of selecting the key dynamic mode of the space mesh antenna oriented to electrical performance is solved.

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  • Electric performance-oriented space mesh antenna key dynamical modal selection method
  • Electric performance-oriented space mesh antenna key dynamical modal selection method
  • Electric performance-oriented space mesh antenna key dynamical modal selection method

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Embodiment Construction

[0062] Attached below figure 1 , To further describe the specific embodiments of the present invention in detail:

[0063] The present invention provides a method for selecting key dynamic modes of a spatial mesh antenna for electrical performance, which includes the following steps:

[0064] Step 1. Input the geometric parameters, material parameters, electrical parameters, and modal cut-off factors of the spatial mesh antenna provided by the user; the geometric parameters include aperture, focal length, offset distance, and minimum distance between front and rear meshes; material parameters include cable structure, The material density, cross-sectional area, Young’s modulus of elasticity, and Poisson’s ratio of the truss structure and the metal wire mesh structure; electrical parameters include operating wavelength, feed parameters, feed primary pattern, and antenna gain, lobe width, Electrical performance requirements including lobe level and pointing accuracy; modal truncation ...

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Abstract

The invention discloses an electric performance-oriented space mesh antenna key dynamical modal selection method. The method comprises the following steps of: inputting geometric parameters, material parameters, electric parameters of modal guillotine factors; calculating an ideal antenna far electric field; establishing an antenna structure finite element model; extracting node, unit and shape function information; calculating a unit electric performance first-order coefficient matrix; grouping an overall electric performance first-order coefficient matrix; carrying out antenna structure modal analysis; outputting a modal matrix; calculating a first-order sensitivity, for the modal, of the electric performance; outputting a modal shape equivalent mass fraction; calculating significance factors, for the modal, of the electric performance; judging whether the significance factors are greater than the modal guillotine factors or not; if the judging result is positive, selecting the significance factors; and otherwise, abandoning the significance factors. According to the method disclosed by the invention, the deficiencies of the traditional dynamical modal selection method are overcome, the influences, on the electric performance of antennas, of modals in different orders are integrally considered in the modal selection process, and the problem of electric performance-oriented space mesh antenna key dynamical modal selection is solved.

Description

Technical field [0001] The invention belongs to the technical field of radar antennas, and particularly relates to a method for selecting key dynamics modes of a space mesh antenna facing electrical performance in the field of radar antennas. Background technique [0002] Mesh antennas are gradually used in the design of space antennas due to their light weight and small size. When the mesh antenna is in orbit, it is periodically affected by dynamic loads such as space radiant heat and impact. The deformation of the antenna surface caused by the dynamic load will cause the antenna structure to vibrate, the electrical performance gain will decrease, the sidelobe level will rise, and the beam tilt will seriously affect the working performance of the antenna. In order to analyze the influence of dynamic load on the electrical performance of the mesh antenna, a dynamic model of the antenna structure needs to be established first. The establishment and analysis of the dynamic model ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
CPCG06F30/23
Inventor 张树新杜敬利张岳震张洁杨东武张逸群
Owner XIDIAN UNIV
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