Anti-interference method of satellite navigation receiver

A technology for satellite navigation and satellite navigation signals, applied in the research field of satellite navigation receiver data processing, can solve the problems of poor anti-interference effect, small data processing amount, unfavorable engineering realization, etc. The effect that is beneficial to the realization of the project

Inactive Publication Date: 2014-12-17
CHENGDUSCEON TECH
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Problems solved by technology

[0046] The invention provides an anti-jamming method for a satellite navigation receiver, which solves the technical problems that the existing anti-jamming method for satellite navigation receivers has a large amount of calculation, is not conducive to engineering realization, has poor real-time performance, and poor anti-jamming effect. The anti-jamming method of the satellite navigation receiver has a small amount of calculation, which is beneficial to the realization of the project, and the data processing amount is small, the real-time performance is good, the stability is good, and the technical effect of the anti-jamming effect is good.

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  • Anti-interference method of satellite navigation receiver
  • Anti-interference method of satellite navigation receiver

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Embodiment 1

[0082] In the first embodiment, a satellite navigation receiver anti-jamming method is provided, please refer to Figure 1-Figure 4 , the method includes:

[0083] Step A: Set up a uniform circular array, the number of antennas is four, and the distance between array elements is d=l / 2, where l is the wavelength of the satellite navigation signal;

[0084] Step B: The array antenna receives and processes satellite navigation signals and interference signals from different directions;

[0085] Step C: Perform delay processing on the four-way signals to obtain M×P-dimensional data units, where M is the number of array units, and P is the number of delay units;

[0086] Step D: Obtain the reference channel and the remaining receiving channel that need to perform the steepest descent algorithm;

[0087] Step E: Set weight parameters and perform filtering;

[0088] Step F: Perform error estimation based on the reference channel to obtain error parameters;

[0089] Step G: Accord...

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Abstract

The invention discloses an anti-interference method of a satellite navigation receiver. The method includes: firstly, setting an array for lineup; receiving signals through an array antenna and processing the signals; conducting delay processing to the signals; obtaining a reference channel and a surplus reception channel; setting a weight parameter for filtering; conducting error estimation to obtain an error parameter; selecting a step length factor for weight updating; repeating until an algorithm enters a steady state convergence point to obtain a weight of the steady state convergence point; utilizing the weight to filter the signals so as to obtain the signals after anti-interference; sending digital signals after anti-interference processing to a rear-end for processing, or sending the digital signals to a DA (digital to analog) converter to be converted to analog signals for outputting. The anti-interference method of the satellite navigation receiver is small in calculation amount, is favorable for a project to be realized, and is small in data processing capacity, and fine in instantaneity, steady state and anti-interference effect.

Description

technical field [0001] The invention relates to the field of satellite navigation receiver data processing research, in particular to an anti-jamming method for a satellite navigation receiver. Background technique [0002] The antenna of the traditional satellite navigation receiver is an omnidirectional single antenna. It does not consider the azimuth of the satellite. While receiving all the navigation signals from the air, it also receives all the interference signals in the covered frequency band. When the interference intensity exceeds the tolerance limit of the receiver , it will seriously affect the performance of the receiver, making its design function impossible to achieve. For this reason, the adaptive nulling antenna is adopted. In actual work, the physical position of the array unit does not change, but through array signal processing, the direction of the interference signal is distinguished in the air domain, and the space-time joint algorithm is used to adap...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01S19/21
CPCG01S19/21
Inventor 幸璐璐董李梅王晓洪吴仡嘉乐王胜伟余湋
Owner CHENGDUSCEON TECH
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