Wide beam circularly-polarized transceiving shared small satellite antenna

A technology for sharing transceivers and satellite antennas, which is applied in the field of satellite antennas. It can solve the problems of narrow beam width of microstrip antennas and the inability to share transceivers with helical antennas. It achieves simple structure and processing technology, improved standing wave and axial ratio characteristics, and small size. Effect

Inactive Publication Date: 2018-02-23
NANJING UNIV OF SCI & TECH
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  • Summary
  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The purpose of the present invention is to provide a small satellite antenna shared by wide-beam circular polarization for transmitting and receiving, which solves the problems that the helical antenna cannot be used for transmitting and receiving, and the beam width of the microstrip antenna is narrow.

Method used

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  • Wide beam circularly-polarized transceiving shared small satellite antenna
  • Wide beam circularly-polarized transceiving shared small satellite antenna
  • Wide beam circularly-polarized transceiving shared small satellite antenna

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Embodiment Construction

[0020] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0021] combine figure 1 , figure 2 , image 3 and Figure 4 , a wide-beam circularly polarized transmitting and receiving shared small satellite antenna, suitable for the wide-beam circularly polarized antenna of a low-orbit small satellite system, in particular to a wide-beam circularly polarized transmitting and receiving shared small satellite antenna working in the S frequency band. It includes a circular metal base plate 1, a metal circular platform 2, a circular radiator 3 and an electric bridge 4; the metal circular platform 2 is a hollow circular platform, forming a three-dimensional grounding structure and a folded conductor wall, and the large bottom surface of the metal circular platform 2 is fixed by screws At the center of the circular metal base plate 1, the top surface of the metal circular platform 2 is fixed to the center of the bottom su...

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Abstract

The invention discloses a wide beam circularly-polarized transceiving shared small satellite antenna, which comprises a circular metal bottom plate, a metal round table, a circular radiator and an electric bridge, wherein the metal round table is a hollow round table, the bottom surface with a large area of the metal round table is fixed at the center of the circular metal bottom plate, the top surface of the metal round table is fixed at the center of the bottom surface of the circular radiator, the diameter of the circular radiator is greater than the diameter of the top surface of the metalround table and is less than the diameter of the circular metal bottom plate, and the electric bridge is arranged inside the metal round table and is fixed to the inner wall of the top surface of themetal round table. According to the wide beam circularly-polarized transceiving shared small satellite antenna, -1dBi gain thereof within a frequency band range can cover a space domain range with apitch angle ranging from -85 to 85 degrees (where 0 degree is on behalf of the antenna axial direction) and an azimuth angle ranging from 0 to 360 degrees; and the wide beam circularly-polarized transceiving shared small satellite antenna has a right-handed circularly-polarized port and a left-handed circularly-polarized port, realizes circularly-polarized transceiving sharing of the antenna, andhas the advantages of small size, light weight, and simple structure and processing technology.

Description

technical field [0001] The invention belongs to the field of satellite antennas, in particular to a small satellite antenna shared by wide-beam circular polarization transceiving. Background technique [0002] Compared with satellites in geosynchronous orbit, low-orbit satellites mainly refer to satellites that run on elliptical orbits and have obvious perigee, and are generally small satellites with small weight and short life. It is mainly used in near-earth communication and measurement occasions that require high resolution accuracy and low signal attenuation, such as surveying and mapping, detection, photography and satellite communication. Due to the obvious perigee of the low-orbit satellite, the electromagnetic wave emitted by the satellite reaches the ground with a very short straight-line distance at this time, which is conducive to sending and receiving with portable devices with low antenna gain and low transmission power. Therefore, it is often used as a satelli...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01Q1/38H01Q1/48H01Q1/50H01P5/18
CPCH01Q1/38H01P5/184H01Q1/48H01Q1/50
Inventor 肖旭夏风琳楚然
Owner NANJING UNIV OF SCI & TECH
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