Low noise GPS (Global Positioning System) carrier wave tracking method based on RSL (Recursive least square filter)

A carrier tracking, low-noise technology, used in radio wave measurement systems, satellite radio beacon positioning systems, measurement devices, etc.

Active Publication Date: 2011-06-15
BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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Problems solved by technology

[0003] The technical solution problem of the present invention is: overcome the deficiency of prior art, provide a kind of low-noise

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  • Low noise GPS (Global Positioning System) carrier wave tracking method based on RSL (Recursive least square filter)
  • Low noise GPS (Global Positioning System) carrier wave tracking method based on RSL (Recursive least square filter)
  • Low noise GPS (Global Positioning System) carrier wave tracking method based on RSL (Recursive least square filter)

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[0026] The specific embodiments of the present invention will be further described in detail below with reference to the accompanying drawings.

[0027] like figure 1 As shown, it is a principle block diagram of the RSL-based low-noise GPS carrier tracking method of the present invention. The steps of the carrier tracking method are as follows:

[0028] (1) The sine signal generated by the satellite digital intermediate frequency signal and the carrier numerically controlled oscillator is mixed by the mixer to generate an in-phase mixing result, and then the in-phase mixing result is multiplied by the C / A code generated by the code generator In order to realize carrier stripping and code stripping, the same-direction sampling signal i(t) is obtained; the C / A code generated by the code generator is a pseudo-random code of GPS satellite, and the code rate is 10.23M.

[0029] The sine signal generated by the carrier numerically controlled oscillator is subjected to a 90-degree ...

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Abstract

The invention relates to a low noise GPS (Global Positioning System) carrier wave tracking method based on an RLS (Recursive least square filter). The low noise GPS carrier wave tracking method comprises the following steps of: measuring an instantaneous phase difference of a local carrier wave and a tracking satellite by a carrier wave tracking loop by utilizing a table look-up type second quadrant arc tangent phase discriminator; introducing the RLS to filter measurement noises; meanwhile estimating a frequency difference according to phase difference variation; utilizing the frequency difference and the phase difference as frequency discrimination input and phase discrimination input of a loop filter with a second order lock frequency loop assistant in a three-order phase locking loop; filtering by the loop filter to output a carrier wave control adjustment variable with high precision and low noise, and correspondingly adjusting carrier wave NCO (Numerical Control Oscillation) to control the local carrier wave so that a receiver keeps phases and frequencies of the local carrier and a tracking satellite carrier wave consistent. In the invention, the low noise GPS carrier wave tracking method based on the RSL ensures that the GPS carrier wave tracking loop can work stably under the condition of low signal to noise ratio and certain dynamic state, keeps the phase not to overturn or skip cycles and ensures the carrier wave tracking precision.

Description

technical field [0001] The invention relates to a low-noise GPS carrier tracking method, in particular to an RSL-based low-noise GPS carrier tracking method. Background technique [0002] For GPS receivers, the acquisition, tracking, and demodulation of satellite signals are the basis of positioning and navigation, and one of its key technologies is the design of carrier tracking loops. The purpose of the carrier tracking loop is to try its best to keep the copied carrier signal consistent with the received satellite carrier signal, so as to completely strip the carrier of the satellite signal through the frequency mixing mechanism. If the copied carrier is inconsistent with the received carrier, the carrier in the received signal cannot be completely stripped, that is to say, the received signal cannot be down-converted to a real baseband signal, which affects the correct extraction of navigation message data bits. In addition, if the consistency between the copied carrier...

Claims

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Application Information

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IPC IPC(8): G01S19/29
Inventor 陈怡聂磊韩琦杨虎刘昌杰包亮
Owner BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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