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-rw-r--r--vorlagen/thesis/src/kapitel_A.tex10
1 files changed, 5 insertions, 5 deletions
diff --git a/vorlagen/thesis/src/kapitel_A.tex b/vorlagen/thesis/src/kapitel_A.tex
index 13bb98d..3fbbb2e 100644
--- a/vorlagen/thesis/src/kapitel_A.tex
+++ b/vorlagen/thesis/src/kapitel_A.tex
@@ -465,7 +465,7 @@ developer to troubleshoot and find the bug.
\begin{tabular}{llll}
\toprule
%$D$&&$P_u$&$\sigma_N$\\
-State&Color \& Pattern&When&Precedence\\\toprule
+\textbf{State}&\textbf{Color \& Pattern}&\textbf{When}&\textbf{Precedence}\\\toprule
Self-test failure&Red - Steady &In boot or application code when a power&1 (High) \\
&&on self-test fails\\\midrule
Unspecified failure&Red - Steady &On software fatal errors&2\\\midrule
@@ -504,7 +504,7 @@ are the RRLP assistance data converted in the RRLP packet generator software.
\begin{tabular}{lllcc}
\toprule
%$D$&&$P_u$&$\sigma_N$\\
-Field (IE) & Description\\\toprule
+\textbf{Field (IE)} & \textbf{Description}\\\toprule
$A_{1}$&Drift coefficient of GPS time scale relative\\
&to UTC time scale\\\midrule
$A_{0}$&Bias coefficient of GPS time scale relative\\
@@ -527,7 +527,7 @@ $\Delta t_{LSF}$&Current of future leap second count
\begin{tabular}{llllc}
\toprule
%$D$&&$P_u$&$\sigma_N$\\
-Field (IE) & Description\\\toprule
+\textbf{Field (IE)} & \textbf{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
@@ -549,7 +549,7 @@ $\beta_{3}$&Coefficient 3 of period of the model
\begin{tabular}{llll}
\toprule
%$D$&&$P_u$&$\sigma_N$\\
-Field (IE) & Description\\\toprule
+\textbf{Field (IE)} & \textbf{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
@@ -598,7 +598,7 @@ Idot&Rate of inclination angle (semicircles/second)
\begin{tabular}{lll}
\toprule
%$D$&&$P_u$&$\sigma_N$\\
-Field (IE) & Description\\\toprule
+\textbf{Field (IE)}& \textbf{Description}\\\toprule
SatelliteID&This is the satellite ID that is in the range of 0 to 63. PRN=SatelliteID + 1\\\midrule
SV Health&Satellite health (e.q. 000 means the satellite is fully operational)\\\midrule
$e$&``Eccentricity shows the amount of the orbit deviation from circular (orbit).\\