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/maindoc.pdf | Bin 6122962 -> 6144285 bytes vorlagen/thesis/src/kapitel_x.tex | 106 +++++++++++++++++++++++++++++++++----- 2 files changed, 93 insertions(+), 13 deletions(-) diff --git a/vorlagen/thesis/maindoc.pdf b/vorlagen/thesis/maindoc.pdf index f847039..cd791e0 100644 Binary files a/vorlagen/thesis/maindoc.pdf and b/vorlagen/thesis/maindoc.pdf differ 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} -- cgit v1.2.3-55-g7522