From f38010542ab7b8b1e16e29cee5545e2402c4cd03 Mon Sep 17 00:00:00 2001
From: Maxime Journot <maxime.journot@csgroup.eu>
Date: Thu, 14 Nov 2024 10:30:13 +0100
Subject: [PATCH] Improved tutorial page
---
doc-tutorials.html | 81 ++++++++++++++++++++++++++++++++++++----------
1 file changed, 64 insertions(+), 17 deletions(-)
diff --git a/doc-tutorials.html b/doc-tutorials.html
index 673e6fb..aad9419 100644
--- a/doc-tutorials.html
+++ b/doc-tutorials.html
@@ -9,10 +9,8 @@ layout: default_orekit
<h2>Java tutorials, by the Orekit team</h2>
-<p>The tests suite is the first place to look for getting help with Orekit
- use.
-
- Some tutorials are provided with source code and comments in order to
+<h3>Markdown tutorials</h3>
+<p>Tutorials provided with source code and comments in order to
emphazise particular use cases:</p>
<ul class="fa-ul">
@@ -62,11 +60,22 @@ layout: default_orekit
</li>
</ul>
-<p>Other tutorials are available on the dedicated <a href="https://gitlab.orekit.org/orekit/orekit-tutorials">Orekit Tutorials</a> project on the forge:</p>
+<h3>Pure Java tutorials</h3>
+<p>You will find the source code of these tutorials on the dedicated <a href="https://gitlab.orekit.org/orekit/orekit-tutorials/-/tree/master/src/main/java/org/orekit/tutorials?ref_type=heads">Orekit Tutorials</a> project on the forge:</p>
+
<ul class="fa-ul">
- <li>Attitude / EarthObservation: shows how to easily switch between day and night attitude modes</li>
+ <li>
+ <span class="fa-li fa-lg fa fa-gears"></span>
+ Attitude
+ <ul>
+ <li>EarthObservation: shows how to easily switch between day and night attitude modes</li>
+ </ul>
+ </li>
<p>
- <li>Bodies
+
+ <li>
+ <span class="fa-li fa-lg fa fa-gears"></span>
+ Bodies
<ul>
<li>DEFile: reads a DEXXX binary file (JPL or IMCCE inpop ephemeris file) and writes a new one containing only the data asked by the user</li>
<li>Phasing: sets up a Sun-synchronous Earth-phased Low Earth Orbit</li>
@@ -74,9 +83,18 @@ layout: default_orekit
</li>
<p>
- <li>Control / indirect / FixedBoundarySingleShooting: shows how to use the indirect (single) shooting method of Orekit. The study case is inspired by the Global Trajectory Optimization Competition 12</li>
+ <li>
+ <span class="fa-li fa-lg fa fa-gears"></span>
+ Control / indirect
+ <ul>
+ <li>FixedBoundarySingleShooting: shows how to use the indirect (single) shooting method of Orekit. The study case is inspired by the Global Trajectory Optimization Competition 12</li>
+ </ul>
+ </li>
<p>
- <li>Conversion
+
+ <li>
+ <span class="fa-li fa-lg fa fa-gears"></span>
+ Conversion
<ul>
<li>PropagatorConversion: helps understand how a propagator can be converted to another with a different model.<br>
Here we convert a numerical propagator into an analytical Keplerian propagator
@@ -86,10 +104,17 @@ layout: default_orekit
</li>
<p>
- <li>Data / Context: explains how to instantiate several data contexts</li>
+ <li>
+ <span class="fa-li fa-lg fa fa-gears"></span>
+ Data
+ <ul>
+ <li>Context: explains how to instantiate several data contexts</li>
+ </ul>
<p>
- <li>Estimation: orbit determination (OD) example
+ <li>
+ <span class="fa-li fa-lg fa fa-gears"></span>
+ Estimation: orbit determination (OD) example
<ul>
<li>DSSTOrbitDetermination: batch least-square OD with a DSST propagator for a MEO (GNSS) satellite with RINEX measurements</li>
<li>GNSSOrbitDetermination: same but with a numerical propagator instead</li>
@@ -105,10 +130,18 @@ layout: default_orekit
</li>
<p>
- <li>Frames / Frames1-2-3: different examples of frame management</li>
+ <li>
+ <span class="fa-li fa-lg fa fa-gears"></span>
+ Frames
+ <ul>
+ <li>Frames1-2-3: different examples of frame management</li>
+ </ul>
+ </li>
<p>
- <li>Gnss:
+ <li>
+ <span class="fa-li fa-lg fa fa-gears"></span>
+ Gnss
<ul>
<li>DOPComputation: shows a basic usage for computing the DOP over a geographic zone and for a period</li>
<li>RinexObservationFile: reading of Rinex observation files</li>
@@ -116,7 +149,9 @@ layout: default_orekit
</li>
<p>
- <li>Maneuvers:
+ <li>
+ <span class="fa-li fa-lg fa fa-gears"></span>
+ Maneuvers
<ul>
<li>ApogeeManeuver: large apogee maneuver with a long (~1h) constant thrust maneuver</li>
<li>ImpulseAtNode: shows how to perform a given impulse maneuver at node</li>
@@ -125,10 +160,17 @@ layout: default_orekit
</li>
<p>
- <li>Models / TidalDisplacements: shows how to compute stations tidal displacements</li>
+ <li>
+ <span class="fa-li fa-lg fa fa-gears"></span>
+ Models
+ <ul>
+ <li>TidalDisplacements: shows how to compute stations tidal displacements</li>
+ </ul>
<p>
- <li>Estimation: orbit determination (OD) example
+ <li>
+ <span class="fa-li fa-lg fa fa-gears"></span>
+ Propagation
<ul>
<li>CovariancePropagation: linear covariance propagation example, starting from a CCSDS OPM (Orbit Parameter Message)</li>
<li>DSSTPropagation: propagation with the DSST propagator</li>
@@ -159,7 +201,12 @@ layout: default_orekit
</ul>
</li>
<p>
- <li>Time / Time1: tutorial for dates support</li>
+ <li>
+ <span class="fa-li fa-lg fa fa-gears"></span>
+ Time
+ <ul>
+ <li>Time1: tutorial for dates support</li>
+ </ul>
</ul>
<h3>Maven site for the Java tutorials</h2>
--
GitLab