Adaptive GNSS positioning method capable of adjusting to ionospheric delay

US10288743B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10288743-B2
Application numberUS-201615316171-A
CountryUS
Kind codeB2
Filing dateAug 15, 2016
Priority dateAug 15, 2016
Publication dateMay 14, 2019
Grant dateMay 14, 2019

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Abstract

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A plurality of GNSS satellite signals feeds the signal processing engine operating in certain processing mode including carrier phase smoothed pseudorange positioning, precise point positioning (PPP), pseudorange differential (DGNSS), and carrier phase differential (RTK). The processing engine calculates two estimates of the ionosphere delay for each satellite: the filtered delay and the instant delay. Comparison of them allows to detect turbulent variation of the ionosphere and adjust parameters of two-parametric dynamic mode which improves positioning precision.

First claim

Opening claim text (preview).

What is claimed is: 1. A satellite navigation positioning method, comprising: receiving n navigation signals from K navigation satellites, wherein the n navigation signals are on at least two different carrier frequencies, and wherein n is at least 8 and K is at least 4; on a processor of a navigation receiver, calculating current coordinates based on the n navigation signals; executing an adaptive positioning algorithm for adjusting parameter z representing a time constant of a rate of variation of ionospheric delay, and a scale factor s, which ranges from 1 to 10 and which relates to a baseline length and solar activity; and correcting the calculated current coordinates based on the adaptive positioning algorithm. 2. The method of claim 1 , further comprising calculating a filtered estimate i(t+1) using parameters τ i and s. 3. The method of claim 2 , further comprising calculating an instant estimate i*(t+1) calculated based on instant carrier phase measurements and instant carrier phase ambiguity estimate. 4. The method of claim 3 , further comprising reducing τ i if the correlation coefficient is less than a threshold value T l . 5. The method of claim 3 , further comprising increasing τ i if the correlation coefficient is greater than a threshold value T l . 6. The method of claim 2 , further comprising calculating a correlation coefficient c ⁡ ( t + 1 ) = 〈 i ⁡ ( t + 1 ) , i * ⁡ ( t + 1 ) 〉  i ⁡ ( t + 1 )  ⁢  i * ⁡ ( t + 1 )  . 7. The method of claim 1 , further comprising increasing s if ∥ i *( t+ 1)∥>∥( t+ 1)∥ is true for five sequential time instances. 8. The method of claim 1 , further comprising decreasing s if ∥ i *( t+ 1)∥<∥ i ( t+ 1)∥ is true for five sequential time instances.

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Classifications

  • using carrier phase measurements, e.g. kinematic positioning; using long or short baseline interferometry · CPC title

  • G01S19/40Primary

    Correcting position, velocity or attitude · CPC title

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What does patent US10288743B2 cover?
A plurality of GNSS satellite signals feeds the signal processing engine operating in certain processing mode including carrier phase smoothed pseudorange positioning, precise point positioning (PPP), pseudorange differential (DGNSS), and carrier phase differential (RTK). The processing engine calculates two estimates of the ionosphere delay for each satellite: the filtered delay and the instan…
Who is the assignee on this patent?
Topcon Positioning Systems Inc
What technology area does this patent fall under?
Primary CPC classification G01S19/40. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue May 14 2019 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).