28 août-1 sept. 2017 Paris (France)
Orbital dynamics: a definition
Florent Deleflie  1@  
1 : Institut de Mécanique Céleste et de Calcul des Ephémérides  (IMCCE)
CNRS, Observatoire de Paris
77 Avenue Denfert Rochereau 75014 PARIS -  France

In this introduction, we will be describing the main issues related to the equations of motion of an artifical satellite. We will de describing the basic principles and general methods to propagate a trajectory over short and long time scales. Each part of this short description will be the subject of further explanations later in the day. 


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