From 6c95f5b12d3ffcb8dac5916263332836e4e4a456 Mon Sep 17 00:00:00 2001
From: Refik Hadzialic
Date: Tue, 31 Jul 2012 19:19:30 +0200
Subject: Assistance data

---
 vorlagen/thesis/src/kapitel_x.tex | 106 +++++++++++++++++++++++++++++++++-----
 1 file changed, 93 insertions(+), 13 deletions(-)

(limited to 'vorlagen/thesis/src/kapitel_x.tex')

diff --git a/vorlagen/thesis/src/kapitel_x.tex b/vorlagen/thesis/src/kapitel_x.tex
index 370a088..ff245df 100644
--- a/vorlagen/thesis/src/kapitel_x.tex
+++ b/vorlagen/thesis/src/kapitel_x.tex
@@ -1855,6 +1855,98 @@ constructed by concatenating the bits required to descibre a variable.
 \end{equation}
 In the following tables 
 NAPISI STA JE NAVIGATION MODEL (EPHEMERIS)
+\begin {table}[tp!]
+\caption{Navigation message content.}
+\label{tbl:navMessage}\centering 
+%\rowcolor{2}{light-gray}{}
+\scriptsize
+\begin{tabular}{clccc}
+\toprule 
+%$D$&&$P_u$&$\sigma_N$\\
+Field (IE) & Description\\\toprule
+Satellite ID&This is the satellite ID that is in the range of 0 to 63. PRN=SatelliteID + 1\\\midrule
+Satellite status&This is an indicator of whether this is a new or existing satellite and whether\\
+&the navigation model is new or the same.\\\midrule
+C/A or P on L2&Code(s) on L2 channel\\\midrule
+URA Index&User range accuracy\\\midrule
+SV Health&Satellite health\\\midrule
+IODC&Issue of data, clock\\\midrule
+L2 P Data flag& \\\midrule
+SF 1 Reserved& \\\midrule
+$T_{GD}$&Estimated group delay differential\\\midrule
+$t_{oc}$&Apparent clock correction\\\midrule
+$a_{f2}$&Apparent clock correction\\\midrule
+$a_{f1}$&Apparent clock correction\\\midrule
+$a_{f0}$&Apparent clock correction\\\midrule
+$C_{rs}$&Ampltitude of the sine harmonic correction term to the orbit radius (meters)\\\midrule
+$\Delta n$&Mean motion difference from computed value (semicircles/sec)\\\midrule
+$M_{0}$&Mean anomaly at reference time (semicircles)\\\midrule
+$C_{uc}$&Ampltitude of the cosine harmonic correction term to the\\
+&argument of latitude (radians)\\\midrule
+$e$&Eccentricity\\\midrule
+$C_{us}$&Amplitude of the sine harmonic correction term to the argument of latitude\\
+&(radians)\\\midrule
+$A^{1/2}$&Square root of semi-major axis (meters)\\\midrule
+$t_{oe}$&Reference time ephemeris\\\midrule
+Fit Interval Flag&\\\midrule
+AODO&Age of data offset\\\midrule
+$C_{ic}$&Amplitude of the cosine harmonic correction term to the angle of inclination\\
+&(radians)\\\midrule
+OMEGA$_0$&Longitude of ascending node of orbit plane at weekly epoch (semicircles)\\\midrule
+$C_{is}$&Amplitude of the cosine harmonic correction term to the angle of inclination\\
+&(radians)\\\midrule
+$i_{0}$&Inclination angle at reference time (semicircles)\\\midrule
+$C_{rc}$&Amplitude of the cosine harmonic correction term to the orbit radius (meters)\\\midrule
+$\omega$&Argument of perigee (semicircles)\\\midrule
+OMEGAdot&Rate of right ascension (semicircles/sec)\\\midrule
+Idot&Rate of inclination angle (semicircles/sec)
+\\\bottomrule
+\end {tabular}
+\end {table}
+
+\begin {table}[tp!]
+\caption{GPS Ionosphere Model}
+\label{tbl:ionoModel}\centering 
+%\rowcolor{2}{light-gray}{}
+\scriptsize
+\begin{tabular}{clccc}
+\toprule 
+%$D$&&$P_u$&$\sigma_N$\\
+Field (IE) & Description\\\toprule
+$\alpha_{0}$&Coefficient 0 of vertical delay\\\midrule
+$\alpha_{1}$&Coefficient 1 of vertical delay\\\midrule
+$\alpha_{2}$&Coefficient 2 of vertical delay\\\midrule
+$\alpha_{3}$&Coefficient 3 of vertical delay\\\midrule
+$\beta_{0}$&Coefficient 0 of period of the model\\\midrule
+$\beta_{1}$&Coefficient 1 of period of the model\\\midrule
+$\beta_{2}$&Coefficient 2 of period of the model\\\midrule
+$\beta_{3}$&Coefficient 3 of period of the model
+\\\bottomrule
+\end {tabular}
+\end {table}
+
+\begin {table}[tp!]
+\caption{Navigation message content.}
+\label{tbl:ionoModel}\centering 
+%\rowcolor{2}{light-gray}{}
+\scriptsize
+\begin{tabular}{clccc}
+\toprule 
+%$D$&&$P_u$&$\sigma_N$\\
+Field (IE) & Description\\\toprule
+$\alpha_{0}$&Coefficient 0 of vertical delay\\\midrule
+$\alpha_{1}$&Coefficient 1 of vertical delay\\\midrule
+$\alpha_{2}$&Coefficient 2 of vertical delay\\\midrule
+$\alpha_{3}$&Coefficient 3 of vertical delay\\\midrule
+$\beta_{0}$&Coefficient 0 of period of the model\\\midrule
+$\beta_{1}$&Coefficient 1 of period of the model\\\midrule
+$\beta_{2}$&Coefficient 2 of period of the model\\\midrule
+$\beta_{3}$&Coefficient 3 of period of the model
+\\\bottomrule
+\end {tabular}
+\end {table}
+
+
 \newpage
 \begin{lstlisting}[label=lst:RRLPAssisPER,
 caption={\textbf{Encoding reference location from ASN.1 to PER}},
@@ -1913,19 +2005,7 @@ D9 1101....
    ....0000  Spare Bits = 0000b
 \end{lstlisting}
 
-\begin {table}[tp!]
-\caption{Navigation message content.}
-\label{tbl:navMessage}\centering 
-%\rowcolor{2}{light-gray}{}
-\begin{tabular}{clccc}
-\toprule 
-%$D$&&$P_u$&$\sigma_N$\\
-Field (IE) & Description\\\toprule
-Satellite ID&This is the satellite ID that is in the range of 0 to 63.\\
-  &PRN=SatelliteID + 1\\\midrule
-\\\bottomrule
-\end {tabular}
-\end {table}
+
 
 \section{RRLP Response}
 
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