A Combined Data and Power Management Infrastructure For Small Satell
In 2009 the need for a suitable onboard computer design arose for the small satellite project at the Institute of Space Systems, University of Stuttgart, Germany. It had to meet the constraints imposed by the small satellite (a 130 kg CubeSat) with its fu
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Jens Eickhoff Editor
A Combined Data and Power Management Infrastructure For Small Satellites
Springer Aerospace Technology
For further volumes: http://www.springer.com/series/8613
Jens Eickhoff Editor
A Combined Data and Power Management Infrastructure For Small Satellites
123
Editor Jens Eickhoff Institut für Raumfahrtsyteme Universität Stuttgart Stuttgart Germany
ISSN 1869-1730 ISBN 978-3-642-35556-1 DOI 10.1007/978-3-642-35557-8
ISSN 1869-1749 (electronic) ISBN 978-3-642-35557-8 (eBook)
Springer Heidelberg New York Dordrecht London Library of Congress Control Number: 2013936520 Springer-Verlag Berlin Heidelberg 2013 This work is subject to copyright. All rights are reserved by the Publisher, whether the whole or part of the material is concerned, specifically the rights of translation, reprinting, reuse of illustrations, recitation, broadcasting, reproduction on microfilms or in any other physical way, and transmission or information storage and retrieval, electronic adaptation, computer software, or by similar or dissimilar methodology now known or hereafter developed. Exempted from this legal reservation are brief excerpts in connection with reviews or scholarly analysis or material supplied specifically for the purpose of being entered and executed on a computer system, for exclusive use by the purchaser of the work. Duplication of this publication or parts thereof is permitted only under the provisions of the Copyright Law of the Publisher’s location, in its current version, and permission for use must always be obtained from Springer. Permissions for use may be obtained through RightsLink at the Copyright Clearance Center. Violations are liable to prosecution under the respective Copyright Law. The use of general descriptive names, registered names, trademarks, service marks, etc. in this publication does not imply, even in the absence of a specific statement, that such names are exempt from the relevant protective laws and regulations and therefore free for general use. While the advice and information in this book are believed to be true and accurate at the date of publication, neither the authors nor the editors nor the publisher can accept any legal responsibility for any errors or omissions that may be made. The publisher makes no warranty, express or implied, with respect to the material contained herein. Cover picture original by Sabine Leib, EADS Cassidian Printed on acid-free paper Springer is part of Springer Science+Business Media (www.springer.com)
Foreword
Innovation is the key for success in technical fields and thus cannot be underestimated in space engineering domains working at the cutting edge of feasibility. Therefore, agile industry is continuously supporting innovative developments extending technical limits or abandoning classical design paths. It is particularly difficult to implement such innovative approaches straightforward in commercial satellite projects, in agency funded productive systems like operational Earth observation missions, or in navigation constella
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