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Satellite antenna polarized closed loop tracking method and device

A satellite antenna and closed-loop tracking technology, applied in the field of satellite communications, can solve the problems of two-way interference of anti-polarization signals and poor communication quality, and achieve the effect of reducing two-way interference problems and improving communication quality.

Active Publication Date: 2016-02-17
北京西鼎众合技术有限公司
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  • Abstract
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AI Technical Summary

Problems solved by technology

[0005] Due to the poor communication quality of automatic satellite communication antenna products currently on the market, and the problem of two-way interference of reverse polarization signals, the present invention proposes a satellite antenna polarization closed-loop tracking method and device

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  • Satellite antenna polarized closed loop tracking method and device

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Embodiment Construction

[0030] The specific embodiments of the invention will be further described below in conjunction with the accompanying drawings. The following examples are only used to illustrate the technical solution of the present invention more clearly, but not to limit the protection scope of the present invention.

[0031] figure 1 It shows a schematic flow chart of a satellite antenna polarization closed-loop tracking method provided by an embodiment of the present invention, including:

[0032] S101. Perform an angle closed loop on the pitch angle, azimuth angle, and polarization angle of the satellite antenna, and adjust the pitch angle, the azimuth angle, and the polarization angle to the first preset angle, the second preset angle, and the polarization angle, respectively. third preset angle;

[0033] S102. Perform polarization step-by-step tracking on the beacon signal of the satellite according to the beacon frequency, and convert the beacon signal into a DC level signal accordi...

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Abstract

The invention discloses a satellite antenna polarized closed loop tracking method and a device. The satellite antenna polarized closed loop tracking method comprises steps performing angle loop closing on a pitch angle, an azimuth and a polarized angle of the satellite antenna, regulating the pitch angle, the azimuth and the polarized angle to a first preset angle, a second preset angle and a third preset angle, performing polarized stepping tracking on a beacon signal of a satellite according to a beacon signal frequency, converting the beacon signal to a DC level signal according to the regulated pitch angle, the azimuth and the polarized angle, and regulating the rotation direction and the rotation angle of the satellite antenna according to the change of the DC level signal. The invention adopts the polarized tracking principle identical to the pitching tracking mode to realize the tracking of the angle closed loop and then the tracking of the signal closed loop, reduces the double-direction interference problem of the reversed polarized signal and improves the communication quality.

Description

technical field [0001] The invention relates to the field of satellite communication, in particular to a satellite antenna polarization closed-loop tracking method and device. Background technique [0002] Most of the automatic satellite communication antenna products on the market currently use the method of automatically calculating the theoretical data of the polarization angle based on the latitude and longitude of the station and the orbital position of the target satellite, and the control system drives the polarization mechanism to rotate to the designated position according to the theoretical value. , some products may correct the theoretical angle of polarization according to the roll angle, but they all belong to the open-loop tracking method. [0003] The polarization closed-loop technology is to improve the polarization isolation of the satellite earth station's transmission, so as not to interfere with the user signal working on another polarization transponder....

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01Q3/38
CPCH01Q3/38
Inventor 王洪成刘白然贺文杰
Owner 北京西鼎众合技术有限公司
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