High-performance RTK processing technological method

A high-performance, high-tech technology, applied in the field of satellite navigation and positioning systems, can solve problems such as time-consuming and computing resources, and achieve the effects of improving fixed rate, high accuracy and reliability, and simplifying algorithms

Active Publication Date: 2019-07-30
江苏北斗星通汽车电子有限公司
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AI Technical Summary

Problems solved by technology

[0002]In the field of high-precision positioning, RTK processing is a calculation-intensive link, and each RTK solution involves large matrix multiplication and inverse operations of double-precision floating points. Very time-consuming and computationally resource-intensive

Method used

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Embodiment Construction

[0018] The following clearly and completely describes the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, but not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0019] A high-performance RTK processing technology method, including establishing ionosphere, troposphere and multipath error models, the specific method is:

[0020] S1: Establish a double-difference RTK observation model to estimate the baseline vector and ionospheric parameters between the user and the reference station in real time;

[0021] For the GNSS dual-frequency measurement data, the vertical ionospheric delay parameters from the receiver to the satellite line and the ionospheric puncture point are obtained through carri...

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Abstract

The invention discloses a high-performance RTK processing technological method. The high-performance RTK processing technological method comprises the following steps: building an ionized layer, a convection layer and a multipath error model. The specific method comprises the following steps: S1, building a double-error RTK observation model, and estimating baseline vectors between a user and a baseline station and parameters of the ionized layer in real time; and carrying out carrier smoothing code pseudo range, hardware delay estimation and inclination-verticality transformation on GNSS double-frequency measurement data to acquire vertical ionized layer delay parameters from a receiver to a puncturing point of a satellite line and the ionized layer; S2, selecting multiple reference points and multiple reference satellites of to-be-measured areas; and S3, avoiding base stations which can easily produce multipath environments, and adopting instrument equipment with multipath error resistance in proper base stations. The RTK initialization accuracy and reliability are higher, the positioning is more accurate, the system cost is reduced, the size is reduced, a fixing ratio of RTK under a complicated environment is increased, an algorithm is simplified, and the cost of RTK is reduced.

Description

technical field [0001] The invention relates to the field of satellite navigation and positioning systems, in particular to a high-performance RTK processing technology method. Background technique [0002] In the field of high-precision positioning, RTK processing is a calculation-intensive link. Each RTK solution involves large matrix multiplication and inversion operations of double-precision floating points, which is very time-consuming and computing resources. Therefore, high-frequency RTK processing has high requirements on the performance of the SOC. At the same time, the baseband receiver also needs to work at a higher frequency to support multiple satellite signals and multiple frequency points. Contents of the invention [0003] In view of the above problems, in order to solve the deficiencies in the prior art, the present invention provides a high-performance RTK processing technology method. [0004] Technical scheme of the present invention is as follows: ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01S19/43
CPCG01S19/43Y02A90/10
Inventor 包学兵崔常福
Owner 江苏北斗星通汽车电子有限公司
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