Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

GNSS receiver high sampling clock difference resolving method

A receiver clock difference and high-sampling technology, applied in the field of satellite navigation and positioning, can solve the problem of increased solution time

Active Publication Date: 2020-06-23
NAT SPACE SCI CENT CAS
View PDF28 Cites 3 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] If you want to obtain the high-sampled receiver clock error, using the traditional method, you need to use high-frequency sampling observations to set up the observation equation when using the traditional method, and use the least square method to combine the receiver clock parameters with other unknown parameters ( Receiver position and carrier phase ambiguity parameters, etc.) to solve together, because the matrix operation, especially the matrix inversion operation involved in the GNSS precise positioning solution is proportional to the observation sampling, it will inevitably cause a sharp increase in the solution time

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • GNSS receiver high sampling clock difference resolving method
  • GNSS receiver high sampling clock difference resolving method
  • GNSS receiver high sampling clock difference resolving method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0056] Such as figure 1 As shown, this embodiment is mainly aimed at the scene of static GNSS receivers on the ground, and proposes a high-sampling clock error calculation method for GNSS receivers. The specific implementation steps are as follows:

[0057] Step 101) Use the traditional method to solve the GNSS Precise Point Positioning (PPP, Precise Point Positioning) on ​​the ground, and the data sampling rate is thinned to a low sampling time interval, which is 30 seconds to 15 minutes in this embodiment.

[0058] The ionosphere-free combination observation equation of GNSS is (Zumberger 1997; Kouba 2001):

[0059]

[0060]

[0061] In the formula,

[0062] is the ionosphere-free combined observation of the carrier phase;

[0063] is the ionosphere-free composite observation value of the code pseudorange;

[0064] is the wavelength of the ionosphere-free combined observation of the carrier phase;

[0065] is the ambiguity of the ionosphere-free combined ob...

Embodiment 2

[0115] Such as figure 2 As shown, this embodiment is mainly aimed at the scenario of a space-borne GNSS receiver on a LEO satellite, and proposes a high-sampling clock error calculation method for a GNSS receiver. The specific implementation steps are as follows:

[0116] Step 201) Using the traditional method to solve the LEO precise orbit determination (POD, Precise Orbit Determination) of the spaceborne GNSS.

[0117] The GNSS ionosphere-free combined observation equation for LEO precise orbit determination is similar to that in step 1, the difference is that there is no tropospheric delay term T j ,Specifically:

[0118]

[0119]

[0120] The implication of each parameter in the formula is identical with embodiment 1.

[0121] In LEO precise orbit determination, the state vector contains six parameters of the satellite orbit (a 0 ,e 0 ,i 0 ,Ω 0 ,ω 0 , M 0 ) and force model parameters (light pressure parameters, atmospheric drag parameters, empirical force pa...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention discloses a GNSS receiver high sampling clock difference calculation method. The method comprises the following steps: performing precise single-point positioning calculation by using observation data of a low-sampling GNSS receiver to obtain a first receiver clock difference at a low-sampling moment, and a receiver position parameter, a tropospheric zenith delay parameter and an ambiguity parameter at the low-sampling moment; acquiring high-sampling parameter values corresponding to the three types of parameters at a high-sampling moment, and calculating a second receiver clockdifference at the high-sampling moment by utilizing the three types of high-sampling parameter values; and utilizing the first receiver clock difference and the second receiver clock difference to calculate the optimized high-sampling receiver clock difference. According to the method, matrix calculation is not needed, an algorithm is simple and easy to implement, a result is stable and reliable,and a calculation speed is high.

Description

technical field [0001] The invention relates to the technical field of satellite navigation and positioning, in particular to a high-sampling clock error calculation method for a GNSS receiver. Background technique [0002] The basis of GNSS (Global Navigation Satellite System) navigation and positioning is the measurement of radio signal propagation time. The basic principle of positioning is to measure the propagation time from the GNSS transmitting satellite to the receiver (which can be converted into propagation distance), and perform space resection to obtain the receiver The spatial three-dimensional position at the antenna. Since the GNSS satellite clock and the user receiver clock are difficult to maintain strict synchronization, the actual measured distance between the GNSS satellite and the receiver includes the influence of the GNSS satellite clock error and the receiver clock error. In absolute positioning, the clock error of GNSS satellites is usually correcte...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
IPC IPC(8): G01S19/25G04R20/04
CPCG01S19/256G04R20/04
Inventor 孟祥广孙越强杜起飞白伟华赵丹阳
Owner NAT SPACE SCI CENT CAS
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products