Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations
This book introduces a stability and control methodology named AeroMech, capable of sizing the primary control effectors of fixed wing subsonic to hypersonic designs of conventional and unconventional configuration layout. Control power demands are h
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Bernd Chudoba
Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations A Generic Approach from Subsonic to Hypersonic Speeds
Springer Aerospace Technology
The Springer Aerospace Technology series is devoted to the technology of aircraft and spacecraft including design, construction, control and the science. The books present the fundamentals and applications in all fields related to aerospace engineering. The topics include aircraft, missiles, space vehicles, aircraft engines, propulsion units and related subjects.
More information about this series at http://www.springer.com/series/8613
Bernd Chudoba
Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations A Generic Approach from Subsonic to Hypersonic Speeds
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Bernd Chudoba Department of Mechanical and Aerospace Engineering The University of Texas at Arlington Arlington, TX, USA
ISSN 1869-1730 ISSN 1869-1749 (electronic) Springer Aerospace Technology ISBN 978-3-030-16855-1 ISBN 978-3-030-16856-8 (eBook) https://doi.org/10.1007/978-3-030-16856-8 © Springer Nature Switzerland AG 2019 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. 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. The publisher, the authors and the editors are safe to assume that the advice and information in this book are believed to be true and accurate at the date of publication. Neither the publisher nor the authors or the editors give a warranty, expressed or implied, with respect to the material contained herein or for any errors or omissions that may have been made. The publisher remains neutral with regard to jurisdictional claims in published maps and institutional affiliations. This Springer imprint is published by the registered company Springer Nature Switzerland AG The registered company address is: Gewerbestrasse 11, 6330 Cham, Switzerland
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Acknowledgements
A number of people cooperated in making this work possible, and I would like to acknowledge their contributions. The presented methodology concept was developed from 1995 to 1999 at Cranfield University, England, as part of a research contract with DaimlerChrysler Aerospace Airbus GmbH under contract number EZ Future Projects 80995517. The research contract was formally funded by the European Supersonic Commercial
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