If you wish to contribute or participate in the discussions about articles you are invited to contact the Editor
Linear observation model for PPP: Difference between revisions
Carlos.Lopez (talk | contribs) No edit summary |
Carlos.Lopez (talk | contribs) No edit summary |
||
Line 7: | Line 7: | ||
|Logo=gAGE | |Logo=gAGE | ||
}} | }} | ||
According to the equations described in the [[Combining pairs of signals and clock definition|combination of pairs of signals]] | According to the equations described in the [[Combining pairs of signals and clock definition|combination of pairs of signals]] | ||
::[[File: Comb_Pairs_Sign_Fig_1.png|none|640px]] | ::[[File: Comb_Pairs_Sign_Fig_1.png|none|640px]] | ||
::[[File: Comb_Pairs_Sign_Fig_2.png|none|640px]] | ::[[File: Comb_Pairs_Sign_Fig_2.png|none|640px]] | ||
Line 32: | Line 33: | ||
Following the same procedure as in [[Code Based Positioning (SPP)]], the linear observation model <math>{\mathbf Y}={\mathbf G}\;{\mathbf X}</math> for the code and carrier measurements can be written as: | Following the same procedure as in [[Code Based Positioning (SPP)]], the linear observation model <math>{\mathbf Y}={\mathbf G}\;{\mathbf X}</math> for the code and carrier measurements can be written as: | ||
* '''Prefit-residuals:''' | * '''Prefit-residuals:''' | ||
:<math> | :<math> | ||
Line 74: | Line 77: | ||
* '''Design matrix''' | * '''Design matrix''' | ||
:<math> | :<math> |
Revision as of 14:00, 5 August 2011
Fundamentals | |
---|---|
Title | Linear observation model for PPP |
Author(s) | J. Sanz Subirana, JM. Juan Zornoza and M. Hernandez-Pajares, University of Catalunia, Spain. |
Level | Medium |
Year of Publication | 2011 |
According to the equations described in the combination of pairs of signals
- [math]\displaystyle{ \qquad \mbox{(1)} }[/math]
the code and carrier measurements in the ionosphere-free combination are modelled as:
- [math]\displaystyle{ \begin{array}{l} R^j_C=\rho^j+c(\delta t-\delta t^j)+T^j+\mathcal{M}_C^j+{\boldsymbol \varepsilon}_{_C}^j\\[0.3cm] \Phi^j_C=\rho^j+c(\delta t-\delta t^j)+T^j+\lambda_N\,w^j+B_C^j+m_{_C}^j+{\boldsymbol \epsilon}_{_C}^j \end{array} \qquad \mbox{(2)} }[/math]
where [math]\displaystyle{ R^j_{_C} }[/math] is the unsmoothed code pseudorange measurement for the [math]\displaystyle{ j-th }[/math] satellite in view and [math]\displaystyle{ \Phi^j_{_C} }[/math] is the corresponding carrier measurement.
Following the same procedure as in Code Based Positioning (SPP), the linear observation model [math]\displaystyle{ {\mathbf Y}={\mathbf G}\;{\mathbf X} }[/math] for the code and carrier measurements can be written as:
- Prefit-residuals:
- [math]\displaystyle{ {\mathbf Y}= \left[ \begin{array}{l} R_{_C}^1-\rho_0^1+c\,\delta t^1-T_0^1\\[0.2cm] \Phi_{_C}^1-\rho_0^1+c\,\delta t^1-T_0^1-\lambda_{_{_N}}\,w^1\\ \vdots\\ R^n_{_C}-\rho_0^n+c\,\delta t^n-T_0^n\\[0.2cm] \Phi^n_{_C}-\rho_0^n+c\,\delta t^n-T_0^n-\lambda_{_{_N}}\,w^n\\ \end{array} \right] \qquad \mbox{(3)} }[/math]
Note: The satellite clock offset [math]\displaystyle{ \delta t^j }[/math] includes the satellite clock relativistic correction due to the orbit eccentricity. The relativistic path range correction is included in the geometric range [math]\displaystyle{ \rho_0^j }[/math].The term [math]\displaystyle{ T_0 }[/math] is the nominal value for the tropospheric correction.
Notice that, and according to the equation
- [math]\displaystyle{ T(E)=T_{z,dry}\cdot M_{dry}(E)+T_{z,wet}\cdot M_{wet}(E) }[/math]
the tropospheric delay in the equation (2) can be decomposed into a nominal term [math]\displaystyle{ T_0(E) }[/math] and the deviation from this nominal [math]\displaystyle{ M_{wet}(E)\,\Delta T_{z,wet} }[/math]. That is:
- [math]\displaystyle{ \begin{array}{l} T(E)=T_0(E)+ M_{wet}(E)\,\Delta T_{z,wet}\\[0.3cm] T_0(E)=T_{z_0,dry}\cdot M_{dry}(E)+T_{z_0,wet}\cdot M_{wet}(E) \end{array} \qquad \mbox{(4)} }[/math]
The mapping factor [math]\displaystyle{ M_{wet}(E) }[/math] is an element of the design matrix (5) and the [math]\displaystyle{ \Delta T_{z,wet} }[/math] is a component of the parameters vector (6):
- Design matrix
- [math]\displaystyle{ {\mathbf G}=\left[ \begin{array}{ccccccccccc} \frac{x_0-x^1}{\rho_0^1} & \frac{y_0-y^1}{\rho_0^1} & \frac{z_0-z^1}{\rho_0^1} &1&M_{wet}&0&...&0&...&0\\ \frac{x_0-x^1}{\rho_0^1} & \frac{y_0-y^1}{\rho_0^1} & \frac{z_0-z^1}{\rho_0^1} &1&M_{wet}&1&...&0&...&0\\ \vdots&\vdots &\vdots&\vdots &\vdots&\vdots & & \vdots& & \vdots\\ \frac{x_0-x^1}{\rho_0^1} & \frac{y_0-y^1}{\rho_0^1} & \frac{z_0-z^1}{\rho_0^1} &1&M_{wet}&0&...&0&...&0\\ \frac{x_0-x^1}{\rho_0^1} & \frac{y_0-y^1}{\rho_0^1} & \frac{z_0-z^1}{\rho_0^1} &1&M_{wet}&0&...&\underbrace{1}_{k}&...&0\\[-0.2cm] \vdots&\vdots &\vdots&\vdots &\vdots&\vdots & & & & \vdots\\ \frac{x_0-x^n}{\rho_0^n} & \frac{y_0-y^n}{\rho_0^n} & \frac{z_0-z^n}{\rho_0^n} &1&M_{wet}&0&...&0&...&0\\ \frac{x_0-x^n}{\rho_0^n} & \frac{y_0-y^n}{\rho_0^n} & \frac{z_0-z^n}{\rho_0^n} &1&M_{wet}&0&...&0&...&1 \end{array} \right] \qquad \mbox{(5)} }[/math]
- Vector parameters (to estimate)
- [math]\displaystyle{ {\mathbf X}=\left[ dx, dy, dz, c\,\delta t, \Delta T_{z,wet}, B_C^1, \cdots, B_C^k, \cdots, B_C^s, \right]^T \qquad \mbox{(6)} }[/math]