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Open-loop Kalman method for intermittent tracking of GNSS signals

An intermittent, Kalman filter technology, applied in satellite radio beacon positioning systems, instruments, measuring devices, etc., can solve the problems of narrow signal traction capture range, reduced power consumption, and large intermittent tracking duty cycle

Active Publication Date: 2019-06-04
NAT UNIV OF DEFENSE TECH
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  • Abstract
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Problems solved by technology

The traditional intermittent tracking method is based on a closed-loop tracking structure. Since the signal traction capture range of the closed-loop structure is narrow, and the final tracking accuracy takes a certain amount of time to converge, the sleep cycle in the intermittent tracking method is required to be short and the active cycle is long.
In this case, the duty cycle of intermittent tracking is usually larger, which affects the performance of power reduction
Although the traditional open-loop tracking method can expand the traction capture range of the signal, the tracking accuracy is poor

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  • Open-loop Kalman method for intermittent tracking of GNSS signals
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  • Open-loop Kalman method for intermittent tracking of GNSS signals

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[0081] In order to make the technical solutions and advantages of the present invention clearer, the present invention will be further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present invention, but not to limit the present invention.

[0082] The embodiment of the present invention proposes an open-loop Kalman method for intermittent tracking of GNSS signals, so as to expand the reacquisition range of intermittent tracking and improve the accuracy of tracking results. In the intermittent tracking of GNSS signals, there are active periods and dormant periods, where the active period is T a , the duration of the sleep period is T s , the sum of the two is T=T a +T s .

[0083] The present invention proposes an open-loop Kalman method for intermittent tracking of GNSS signals. The open-loop estimator in the present invention is us...

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Abstract

In the traditional closed-loop intermittent tracking method, it takes a certain amount of time to ensure signal convergence due to the narrow signal traction capture range of the closed-loop structure and the final tracking accuracy. Aiming at the above-mentioned problems in the prior art, the present invention proposes an open-loop Kalman method for intermittent tracking of GNSS signals. The open-loop estimator in the present invention is used for estimating the signal parameters in the active period. In GNSS signal intermittent tracking, there are signal active periods and dormant periods, wherein the duration of the active period is Ta, the duration of the dormant period is Ts, and the sum of the two is T=Ta+Ts. The present invention uses an open-loop estimator to estimate the parameters of the signal in each active cycle in the active cycle of the GNSS signal intermittent tracking, and then uses a Kalman filter to filter the estimation results in different active cycles. Therefore, while expanding the range of signal capture, the precision of signal tracking is also improved.

Description

technical field [0001] The invention relates to the field of navigation receiver equipment development, in particular to an open-loop Kalman method for intermittent tracking of GNSS signals, which can be used in the development of receiving terminal equipment in a satellite navigation system. Background technique [0002] With the popularization of GNSS receiver modules in consumer electronic products, the power consumption of GNSS receivers has become an important index reference. In order to reduce the power consumption of receivers, intermittent tracking technology has received extensive attention and applications. The traditional intermittent tracking method is based on the closed-loop tracking structure. Because the signal traction capture range of the closed-loop structure is narrow, and the final tracking accuracy needs a certain time to converge, the intermittent tracking method requires a short sleep period and a long active period. As a result, the duty cycle of in...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01S19/29G01S19/30
CPCG01S19/29G01S19/30
Inventor 陈雷林红磊唐小妹黄仰博欧钢左勇刘哲李蓬蓬孙鹏跃
Owner NAT UNIV OF DEFENSE TECH