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Anti-interference method and device for navigation receiver through employing inertial navigation equipment

A technology of inertial navigation equipment and navigation receiver, which is applied in the field of electronic information, can solve the problems of not being able to adjust the beam pointing of satellite signals, and not taking into account the enhancement of satellite signals, so as to achieve the effect of enhancing signal receiving gain and weakening interference

Inactive Publication Date: 2016-02-24
湖南中森通信科技有限公司
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Problems solved by technology

However, there are obvious defects in the above two types of schemes: in the first type of scheme, the adaptive processing technology based on nulling only considers interference suppression, and does not take into account the enhancement of satellite signals, so this type of method does not need to predict the direction of satellite signals.
However, in practical applications, since the direction of satellite signals cannot be predicted, the array antenna is usually used to simulate multiple beams, so that each beam points to a different direction divided in advance, so that the synthetic beam can cover the entire upper hemisphere, so that each satellite can be detected. Corresponding beam coverage; therefore, the beam pointing used in the prior art is pre-divided, and the beam pointing cannot be adaptively adjusted according to the satellite signal during actual operation

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  • Anti-interference method and device for navigation receiver through employing inertial navigation equipment
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  • Anti-interference method and device for navigation receiver through employing inertial navigation equipment

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Embodiment Construction

[0037] The invention calculates the steering vector between the satellite and the antenna array according to the information provided by the inertial navigation, and adjusts the weighted weight of the array to form a beam so that it points to the direction of the satellite signal. See attached figure 1 , the device comprises a computing unit 1 connected in sequence, a preset unit 2, a statistical unit 3, an inversion unit 4, a weighting unit 5, a receiving unit 6, a modulating unit 7, and a determining unit 8; the device uses the computing unit 1 and the preset unit 2 Calculate the steering vector.

[0038] In particular, those skilled in the art can make several modifications and improvements without departing from the concept of the present invention, and these all belong to the protection scope of the present invention. Therefore, the protection scope of the patent for the present invention should be based on the appended claims.

[0039] The calculation process of the we...

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Abstract

The invention relates to the technical field of electronic information, specifically an anti-interference method and device for a navigation receiver through employing inertial navigation equipment under the condition of cold start. The method comprises the steps: calculating a guide vector between a satellite and an antenna array according to information provided by inertial navigation, adjusting the weight of an array and forming a wave beam, and enabling the wave beam to face the incoming direction of a satellite signal. The method is advantageous in that 1, the method can divide the direction of the wave beam in an adaptive manner; 2, the method controls the direction of the wave beam synthesized by a plurality of antennas through the position information obtained by the inertial navigation equipment, and achieves the effects of improving signal receiving gain, and weakening interference.

Description

technical field [0001] The invention relates to the technical field of electronic information, in particular to a method and device for anti-interference of a navigation receiver using inertial navigation equipment under cold start. Background technique [0002] It is known that the satellite navigation system is a satellite-based radio navigation system that uses artificial satellites as navigation stations. Due to the low power of the signal sent by the satellite navigation system, it faces a complex and harsh channel environment and is susceptible to various forms of intentional or unintentional interference. It leads to the decline of the navigation and positioning performance of the navigation receiver. Therefore, measures must be taken to combat these interferences to ensure the positioning performance of the navigation receiver. [0003] At present, satellite navigation receivers mainly use adaptive airspace or joint space-time filtering, which are mainly divided into...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01S19/21
CPCG01S19/21
Inventor 吴天笑郑五星
Owner 湖南中森通信科技有限公司
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