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Carrier-smoothing of code pseudoranges: Difference between revisions
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{{Article Infobox2 | {{Article Infobox2 | ||
|Category=Fundamentals | |Category=Fundamentals | ||
|Authors=J. Sanz Subirana, J.M. Juan Zornoza and M. Hernández-Pajares, Technical University of Catalonia, Spain. | |||
|Level=Advanced | |||
|YearOfPublication=2011 | |||
|Title={{PAGENAME}} | |Title={{PAGENAME}} | ||
}} | }} | ||
The noisy (but unambiguous) code pseudorange measurements can be smoothed with the precise (but ambiguous) carrier phase measurements. A simple algorithm (the Hatch filter) is given as follows: | The noisy (but unambiguous) code pseudorange measurements can be smoothed with the precise (but ambiguous) carrier phase measurements. A simple algorithm (the Hatch filter) is given as follows: | ||
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::<math> | ::<math> | ||
\widehat{R}(s;k)= \frac{1}{n} R(s;k)+ \frac{n-1}{n} \left [\widehat{R}(s;k-1)+ \left( \Phi(s;k)-\Phi(s;k-1) \right) \right ] | |||
\widehat{R}(s;k)= \frac{1}{n} R(s;k)+ \frac{n-1}{n} \left [\widehat{R}(s;k-1)+ \left( \Phi(s;k)-\Phi(s;k-1) \right) \right ]\ | \qquad \mbox{(1)} | ||
\mbox{The algorithm is initialised with: | </math> | ||
: The algorithm is initialised with: | |||
::<math> | |||
\widehat{R}(s;1)= R(s;1) | \widehat{R}(s;1)= R(s;1) | ||
</math> | </math> | ||
where, <math>n=k</math> when <math>k<N</math> and <math>n=N</math> when <math>k \geq N</math> | where, <math>n=k</math> when <math>k<N</math> and <math>n=N</math> when <math>k \geq N.</math> | ||
This algorithm must be initialised every time that a carrier phase cycle-slip occurs. | This algorithm must be initialised every time that a carrier phase cycle-slip occurs. | ||
The previous algorithm can be interpreted as a real-time alignment of the carrier phase to the code measurement. That is: | The previous algorithm can be interpreted as a real-time alignment of the carrier phase to the code measurement. That is: | ||
::<math> | ::<math> | ||
\begin{array}{ll} | \begin{array}{ll} | ||
\widehat{R} | \widehat{R}(k)&= \frac{1}{n} R(k)+ \frac{n-1}{n} \left [ \widehat{R}(k-1)+ \left( \Phi(k) - \Phi(k-1) \right) \right ]=\\[0.3cm] | ||
&= \Phi(k) +\frac{n-1}{n} \left (\widehat{R}(k-1)-\Phi(k-1)\right )+ \frac{1}{n} \left( R(k)-\Phi(k) \right)=\\[0.3cm] | |||
&= \ | & =\Phi(k) + \frac{n-1}{n} <R - \Phi>_{(k-1)} + \frac{1}{n} \left ( R(k) - \Phi(k) \right )=\\[0.3cm] | ||
&= | &= \Phi(k) + < R - \Phi >_{(k)} | ||
\end{array} \qquad \mbox{(2)} | \end{array} \qquad \mbox{(2)} | ||
</math> | </math> | ||
where the mean bias <ref group="footnotes">The mean value of a set of measurements <math>\{x_1,\cdots,x_n\}</math> can be computed recursively as: <math><x>_k= \frac{1}{k} x_k+ \frac{k-1}{k}<x>_{k-1}</math>. The equation (2) is a variant of previous expression, that provides an estimate of a moving average over a <math>N</math> samples window. Notice that, when <math>k \geq N</math>, the weighting factors <math>\frac{1}{N}</math> and <math>\frac{N-1}{N}</math> are used instead of <math>\frac{1}{k}</math> and <math>\frac{k-1}{k}</math>.</ref> <math> < R - \Phi > </math> between the code and carrier phase is estimated in real time and used to align the carrier phase with the code. | |||
where the mean bias <ref group="footnotes">The mean value of a set of measurements | |||
For more information, please go to the article: | For more information, please go to the article: | ||
* [[ | * [[Code-Carrier Divergence Effect]] | ||
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[[Category:Fundamentals]] | [[Category:Fundamentals]] | ||
[[Category:GNSS Measurements and Data Preprocessing]] |
Latest revision as of 11:25, 23 February 2012
Fundamentals | |
---|---|
Title | Carrier-smoothing of code pseudoranges |
Author(s) | J. Sanz Subirana, J.M. Juan Zornoza and M. Hernández-Pajares, Technical University of Catalonia, Spain. |
Level | Advanced |
Year of Publication | 2011 |
The noisy (but unambiguous) code pseudorange measurements can be smoothed with the precise (but ambiguous) carrier phase measurements. A simple algorithm (the Hatch filter) is given as follows:
Let's [math]\displaystyle{ R(s;n) }[/math] and [math]\displaystyle{ \Phi(s;n) }[/math] the code and carrier measurement of a given satellite [math]\displaystyle{ s }[/math] at the time [math]\displaystyle{ n }[/math]. Thence, the smoothed code [math]\displaystyle{ \hat{R}(s;n) }[/math] can be computed as:
- [math]\displaystyle{ \widehat{R}(s;k)= \frac{1}{n} R(s;k)+ \frac{n-1}{n} \left [\widehat{R}(s;k-1)+ \left( \Phi(s;k)-\Phi(s;k-1) \right) \right ] \qquad \mbox{(1)} }[/math]
- The algorithm is initialised with:
- [math]\displaystyle{ \widehat{R}(s;1)= R(s;1) }[/math]
where, [math]\displaystyle{ n=k }[/math] when [math]\displaystyle{ k\lt N }[/math] and [math]\displaystyle{ n=N }[/math] when [math]\displaystyle{ k \geq N. }[/math]
This algorithm must be initialised every time that a carrier phase cycle-slip occurs.
The previous algorithm can be interpreted as a real-time alignment of the carrier phase to the code measurement. That is:
- [math]\displaystyle{ \begin{array}{ll} \widehat{R}(k)&= \frac{1}{n} R(k)+ \frac{n-1}{n} \left [ \widehat{R}(k-1)+ \left( \Phi(k) - \Phi(k-1) \right) \right ]=\\[0.3cm] &= \Phi(k) +\frac{n-1}{n} \left (\widehat{R}(k-1)-\Phi(k-1)\right )+ \frac{1}{n} \left( R(k)-\Phi(k) \right)=\\[0.3cm] & =\Phi(k) + \frac{n-1}{n} \lt R - \Phi\gt _{(k-1)} + \frac{1}{n} \left ( R(k) - \Phi(k) \right )=\\[0.3cm] &= \Phi(k) + \lt R - \Phi \gt _{(k)} \end{array} \qquad \mbox{(2)} }[/math]
where the mean bias [footnotes 1] [math]\displaystyle{ \lt R - \Phi \gt }[/math] between the code and carrier phase is estimated in real time and used to align the carrier phase with the code.
For more information, please go to the article:
Notes
- ^ The mean value of a set of measurements [math]\displaystyle{ \{x_1,\cdots,x_n\} }[/math] can be computed recursively as: [math]\displaystyle{ \lt x\gt _k= \frac{1}{k} x_k+ \frac{k-1}{k}\lt x\gt _{k-1} }[/math]. The equation (2) is a variant of previous expression, that provides an estimate of a moving average over a [math]\displaystyle{ N }[/math] samples window. Notice that, when [math]\displaystyle{ k \geq N }[/math], the weighting factors [math]\displaystyle{ \frac{1}{N} }[/math] and [math]\displaystyle{ \frac{N-1}{N} }[/math] are used instead of [math]\displaystyle{ \frac{1}{k} }[/math] and [math]\displaystyle{ \frac{k-1}{k} }[/math].