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Aimed at students, faculty and professionals in the aerospace
field, this book provides practical information on the development,
analysis, and control of a single and/or multiple spacecraft in
space. This book is divided into two major sections: single and
multiple satellite motion. The first section analyses the orbital
mechanics, orbital perturbations, and attitude dynamics of a single
satellite around the Earth. Using the knowledge of a single
satellite motion, the translation of a group of satellites called
formation flying or constellation is explained. Formation flying
has been one of the main research topics over the last few years
and this book explains different control approaches to control the
satellite attitude motion and/or to maintain the constellation
together. The control schemes are explained in the discrete domain
such that it can be easily implemented on the computer on board the
satellite. The key objective of this book is to show the reader the
practical and the implementation process in the discrete domain.
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