From e6b6600882d83295e8b356e145baa3889f800d21 Mon Sep 17 00:00:00 2001 From: =?UTF-8?q?S=C3=A9bastien=20Dinot?= <sebastien.dinot@csgroup.eu> Date: Fri, 27 Oct 2023 09:19:53 +0200 Subject: [PATCH] =?UTF-8?q?Get=20rid=20of=20wrong=20acronym=E2=80=A6?= MIME-Version: 1.0 Content-Type: text/plain; charset=UTF-8 Content-Transfer-Encoding: 8bit --- governance.html | 8 ++++---- 1 file changed, 4 insertions(+), 4 deletions(-) diff --git a/governance.html b/governance.html index 79c919b..610a466 100644 --- a/governance.html +++ b/governance.html @@ -85,10 +85,10 @@ layout: default_orekit <h1 data-number="1" id="introduction"><span class="header-section-number">1</span> Introduction</h1> -<p>OREKIT (ORbits Extrapolation KIT) is a free low level space dynamics - library written in Java. It provides basic elements (orbits, dates, - attitude, frames…) and various algorithms to handle them (conversions, - analytical and numerical propagation, pointing…).</p> +<p>OREKIT is a free low level space dynamics library written in Java. It + provides basic elements (orbits, dates, attitude, frames…) and various + algorithms to handle them (conversions, analytical and numerical + propagation, pointing…).</p> <p>OREKIT is developed under APACHE V2.0 license. All contributions to OREKIT have to be compliant with the terms and conditions of this license. This license belongs to the “Business Friendly” category. It -- GitLab