Method for evaluating compatibility between low-orbit navigation system and medium-high orbit navigation system

A navigation system, medium and high orbit technology, applied in the field of satellite navigation and positioning, can solve the problems of high transmission power, deviation, and the influence of Doppler frequency shift on spectrum separation coefficient is not considered, and achieves equivalent carrier-to-noise ratio attenuation, The effect of reducing bias

Active Publication Date: 2019-08-23
火眼位置数智科技服务有限公司
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Problems solved by technology

[0004] How to evaluate the signal interference between different navigation systems, the current common practice is to use the equivalent carrier-to-noise ratio attenuation as an evaluation index, but the current equivalent carrier-to-noise ratio The analysis method does not take into account the real power spectral density function of the short code signal, but only uses the power spectral density envelope, resulting in a large deviation between the analysis results and the real situation; The influence of the coefficient; the current analysis method generally takes the extreme situation of system interference for analysis, such as taking the shortest interference distance and the largest transmission power, but this analysis method cannot give real interference results within a period of time

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  • Method for evaluating compatibility between low-orbit navigation system and medium-high orbit navigation system

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Embodiment Construction

[0052] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments. Apparently, the described embodiments are some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts shall fall within the protection scope of the present invention.

[0053] like figure 1 As shown, the present invention relates to a compatibility evaluation method between a low-orbit navigation system and a middle-high orbit navigation system, comprising the following steps:

[0054] Step 1. Establish a system scenario through MATLAB and STK software, including generating a low-orbit navigation (LEO) satellite constellation, a medium-high orbit navigation system (Glonass) satellite constellation, and establishing a ground navigation receiver. The specific steps are:

[0055] Step 101: Combine MA...

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Abstract

The invention relates to a method for evaluating compatibility between a low-orbit navigation system and a medium-high orbit navigation system; the method comprises the steps of 1) establishing a low-orbit navigation system satellite constellation, a medium-high orbit navigation system satellite constellation by utilizing MATLAB and STK software, and establishing a ground navigation receiver; 2) traversing all satellites of the two system satellite constellations, and calculating the satellite-to-ground relative distance between the satellites and the receiver; 3) calculating the Doppler frequency shift of the satellite signals of the low-orbit navigation system and the medium-high orbit navigation system; 4) calculating a spectral separation coefficient between signals according to the power spectral density and the corresponding Doppler frequency shift of the two signals; 5) calculating an interference signal to ground power; 6) calculating equivalent carrier-to-noise ratio attenuation at the moment; and 7) calculating the equivalent carrier-to-noise ratio attenuation values of all traversed elements in the whole simulation period, and enabling the interference values of all thestations to be subjected to compatibility evaluation. Compared with the prior art, the method has the advantages that a more real interference result can be obtained, and the deviation between an analysis result and a real condition is reduced.

Description

technical field [0001] The invention relates to the technical field of satellite navigation and positioning, in particular to a compatibility evaluation method between a low-orbit navigation system and a mid-high orbit navigation system. Background technique [0002] Global Navigation Satellite System (GNSS), especially the GPS system of the United States, the GLONASS system of Russia, the Galileo system of Europe and the Beidou system of China, have been widely used in the world and provide navigation and positioning services for users in various fields . With the promotion of applications, the current high-precision surveying and mapping, precision agriculture, transportation and logistics transportation, aviation management and other fields have higher and higher requirements for the accuracy, availability, and integrity of navigation and positioning. The traditional GNSS system can no longer meet the needs. Using low-orbit satellites Due to its own characteristics, the ...

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Application Information

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IPC IPC(8): G01S19/23G01S19/21G01S19/20
CPCG01S19/23G01S19/21G01S19/20
Inventor张悦江金凤
Owner火眼位置数智科技服务有限公司