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Quadratic quantization method of satellite-borne receiver and satellite-borne receiver thereof

A space-borne receiver and secondary quantization technology, applied in radio transmission systems, electrical components, transmission systems, etc., can solve problems such as large resource consumption, loss of useful signals, and complex logic judgments, achieving low resource consumption and low cost , logical judgment simple effect

Pending Publication Date: 2021-07-13
NAT UNIV OF DEFENSE TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For this reason, the present invention proposes a secondary quantization method for an on-board receiver and its on-board receiver, which can solve the problems of useful signal loss, large resource consumption, and complex logic judgments caused by existing time-domain anti-jamming methods

Method used

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  • Quadratic quantization method of satellite-borne receiver and satellite-borne receiver thereof
  • Quadratic quantization method of satellite-borne receiver and satellite-borne receiver thereof

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Embodiment Construction

[0020] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals designate the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.

[0021] In the description of the present invention, unless otherwise clearly defined, words such as setting, installation, and connection should be understood in a broad sense, and those skilled in the art can reasonably determine the specific meanings of the above words in the present invention in combination with the specific content of the technical solution.

[0022] refer to figure 2 , a secondary quantization method for a spaceborne receiver, comprising the following steps:

[0023] S1, AGC adaptively adjusts a reasonable gain to...

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Abstract

The invention discloses a secondary quantization method of a satellite-borne receiver and the satellite-borne receiver, aiming at the defects of a time domain anti-interference technology, amplitude amplification is carried out on a baseband signal subjected to down-conversion, and then a high order is intercepted, so that the secondary quantization method can adapt to the stability of anti-interference in a large dynamic range; meanwhile, the method ingeniously and effectively suppresses the pulse interference while suppressing the continuous wave interference, is a zero-resource-consumption method for the pulse interference, is low in cost and easy to implement, and can effectively solve the problems of useful signal loss, large resource consumption and complex logic judgment caused by a time domain anti-interference technology.

Description

technical field [0001] The invention relates to the technical field of satellite-borne signal processing, in particular to a secondary quantization method of a satellite-borne receiver and the satellite-borne receiver thereof. Background technique [0002] The increasing complexity of the space electromagnetic environment makes interference more and more complex, and the stability and reliability of spaceborne receivers are seriously affected. In order to suppress various interferences, the anti-jamming technology of spaceborne receivers continues to develop. For the time-domain anti-jamming technology, especially when pulse interference and continuous wave interference exist at the same time, the time-domain narrowband interference suppression technology includes two methods: linear and nonlinear, both of which are based on adaptive filtering and subspace decomposition. CW has a good suppression effect, but it has little effect on pulse interference due to the long converge...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04B7/185H04B1/12
CPCH04B7/18502H04B1/12
Inventor 黄龙鲁祖坤都倩倩李柏渝刘哲吴健周彦波周海洋邱杨杨威
Owner NAT UNIV OF DEFENSE TECH
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