E-Book Overview
This book covers all aspects of inertial navigation systems (INS), including the sensor technology and the estimation of instrument errors, as well as their integration with the Global Positioning System (GPS) for geodetic applications. Complete mathematical derivations are given. Both stabilized and strapdown mechanizations are treated in detail. Derived algorithms to process sensor data and a comprehensive explanation of the error dynamics provide not only an analytical understanding but also a practical implementation of the concepts. A self-contained description of GPS, with emphasis on kinematic applications, is one of the highlights in this book.The text is of interestto geodesists, including surveyors, mappers, and photogrammetrists; to engineers in aviation, navigation, guidance, transportation, and robotics; and to scientists involved in aerogeophysics and remote sensing.
E-Book Content
Christopher Jekeli
Inertial Navigation Systems with Geodetic Applications
Walter de Gruyter Berlin New York 2001
Author
Dr. Christopher Jekeli Department of Civil & Environmental Engineering & Geodetic Science The Ohio State University 470 Hitchcock Hall, 2070 Neil Avenue Columbus, Ohio 43210-1275 USA
@Printed on acid-free paper which falls within the guidelines of the ANSI to ensure permanence and durability.
Library
of Congress Cataloging-in-Publication Data
Jekeli, Christopher, 1953Inertial navigation systems with geodetic applications / Christopher Jekeli. p. cm. Includes bibliographical references and index. ISBN 3110159031 1. Earth - Figure - Measurement. 2. Inertial navigation Mathematics. I. Title. QB283 ,545 2001 526’.1 -dc21 00-03 1644
Die Deutsche Bibliothek - Cataloging-in-Publication Data
Jekeli, Christopher: Inertial navigation systems with geodetic applications I Christopher Jekeli. - Berlin ; New York : de Gruyter, 2001 ISBN 3-11-015903-l
0 Copyright 2000 by Walter de Gruyter GmbH & Co. KG, 10785 Berlin, Germany All rights reserved, including those of translation into foreign languages. No part of this book may be reproduced or transmitted in any form or by any means, electronic or mechanical, including photocopy, recording or any information storage and retrieval system, without permission in writing from the publisher. Cover design: Rudolf Hiibler, Berlin Typesetting: ASCO Trade Typesetting Ltd., Hong Kong Printing: Werner Hildebrand, Berlin Binding: Liideritz & Bauer-GmbH, Berlin
To my Mother and Father
Preface
It is amazing that gyros perform as well as they do.
Wallace E. Vander Velde, M.I.T., 1983. The quote above is a beautiful expression and tribute to the engineering triumph in the latter half of the twentieth century of the mechanical gyroscope that is an integral part of the traditional inertial navigation system (INS). In today’s technological age of lasers and digital electronics, having also benefited inertial sensors, high performance is almost expected; yet the most accurate navigation and guidance systems still rely on the mechanical predecessors of the modern optical gyro. On the other hand, robustness, reliability, efficiency, and, above all, cost-effectiveness belong to the new generation of sensors and open the opportunity for increased utility and wider application in commercial, industrial, and scientific endeavors, Concurrent with the technological innovations came new analytical tools, specifically the Kalman filter, that is tailor-made for the analysis, calibration, and integration of the inertial navigation system. In the last two decades, the Global Positioning System (GPS) has come to dominate the wide range of positioning and navigation applications, but the new inertial sensor technology has enabled a continuing and growing utilization of these marvelous instru