ebook img

Spacecraft Dynamics PDF

454 Pages·2005·56.468 MB·English
Save to my drive
Quick download
Download
Most books are stored in the elastic cloud where traffic is expensive. For this reason, we have a limit on daily download.

Preview Spacecraft Dynamics

SPACECRAFT DYNAMICS Thomas R. Kane, Peter W Likins,. and David A. Levinson Spacecraft Dynamics Thomas R. Kane, Stanford University Peter W. Likins, Lehigh University David A. Levinson, Lockheed Palo Alto Research Laboratory Copyright 2005 by the authors Previously published by McGraw-Hill Book Company, 1993 Now published by The Internet-First University Press This manuscript is among the initial offerings being published as part of a new approach to scholarly publishing. The manuscript is freely available from the Internet-First University Press repository within DSpace at Cornell University at: http://dspace.library.cornell.edu/handle/1813/62 The online version of this work is available on an open access basis, without fees or restrictions on personal use. A professionally printed and bound version may be purchased through Cornell Business Services by contacting: [email protected] All mass reproduction, even for educational or not-for- profit use, requires permission and license. For more information, please contact [email protected]. Ithaca, N.Y. January 2005 £NGJN. MOV 1 1982 CORNELL UNIVERSITY LIBRARIES ITHACA, N. Y. 14853 Engineering Library Carpenter Hall SPACECRAFT DYNAMICS Thomas R. Kane Stanford University Peter W. Likins Lehigh University David A. Levinson Lockheed Palo Alto Research Laboratory McGraw-Hill Book Company New York St. Louis San Francisco Auckland Bogota Hamburg Johannesburg London Madrid Mexico Montreal New Delhi Panama Paris Sao Paulo Singapore Sydney Tokyo Toronto This book was set in Times Roman by Andover Graphics. The editors were Diane D. Heiberg and Madelaine Eichberg; the production supervisor was Leroy A. Young. New drawings were done by Danmark & Michaels, Inc. The cover was designed by Mark Wieboldt. Halliday Lithograph Corporation was printer and binder. SPACECRAFT DYNAMICS Copyright © 1983 by McGraw-Hill, Inc. All rights reserved. Printed in the United States of America. Except as permitted under the United States Copyright Act of 1976, no part of this publication may be reproduced or distributed in any form or by any means, or stored in a data base or retrieval system, without the prior written permission of the publisher. 1234567890 HDHD 898765432 ISBN 0-Q7-Q37flM3-b Library of Congress Cataloging in Publication Data Kane, Thomas R. Spacecraft dynamics. Includes index. 1. Space vehicles—Dynamics. I. Likins, Peter W. II. Levinson, David A. III. Title. TL1050.K36 629.47'0r53111 81-8431 ISBN 0-07-037843-6 AACR2 j> CONTENTS Preface vii To the Reader xi Chapter 1 Kinematics 1 1.1 Simple Rotation 1 1.2 Direction Cosines 4 1.3 Euler Parameters 12 1.4 Rodrigues Parameters 16 1.5 Indirect Determination of Orientation 20 1.6 Successive Rotations 23 1.7 Orientation Angles 30 1.8 Small Rotations 38 1.9 Screw Motion 42 .10 Angular Velocity Matrix 47 .11 Angular Velocity Vector 49 .12 Angular Velocity Components 53 .13 Angular Velocity and Euler Parameters 58 .14 Angular Velocity and Rodrigues Parameters 62 .15 Indirect Determination of Angular Velocity 68 .16 Auxiliary Reference Frames 71 .17 Angular Velocity and Orientation Angles 73 .18 Slow, Small Rotational Motions 78 .19 Instantaneous Axis 81 .20 Angular Acceleration 84 l.21 Partial Angular Velocities and Partial Velocities 87 iii iv CONTENTS Chapter 2 Gravitational Forces 2.1 Gravitational Interaction of Two Particles 2.2 Force Exerted on a Body by a Particle 2.3 Force Exerted on a Small Body by a Particle 2.4 Force Exerted on a Small Body by a Small Body 2.5 Centrobaric Bodies 2.6 Moment Exerted on a Body by a Particle 2.7 Moment Exerted on a Small Body by a Small Body 2.8 Proximate Bodies 2.9 Differentiation with Respect to a Vector 2.10 Force Function for Two Particles 2.11 Force Function for a Body and a Particle 2.12 Force Function for a Small Body and a Particle 2.13 Force Function in Terms of Legendre Polynomials 2.14 Force Function for Two Small Bodies 2.15 Force Function for a Centrobaric Body 2.16 Force Function for a Body and a Small Body 2.17 Force Function Expressions for the Moment Exerted on a Body by a Particle 2.18 Force Function Expression for the Moment Exerted on a Small Body by a Body Chapter 3 Simple Spacecraft 3.1 Rotational Motion of a Torque-Free, Axisymmetric Rigid Body 3.2 Effect of a Gravitational Moment on an Axisymmetric Rigid Body in a Circular Orbit 3.3 Influence of Orbit Eccentricity on the Rotational Motion of an Axisymmetric Rigid Body 3.4 Torque-Free Motion of an Unsymmetric Rigid Body 3.5 Effect of a Gravitational Moment on an Unsymmetric Rigid Body in a Circular Orbit 3.6 Angular Momentum, Inertia Torque, and Kinetic Energy of a Gyrostat 3.7 Dynamical Equations for a Simple Gyrostat 3.8 Rotational Motion of a Torque-Free, Axisymmetric Gyrostat 3.9 Reorientation of a Torque-Free Gyrostat Initially at Rest 3.10 Effect of a Gravitational Moment on an Axisymmetric Gyrostat in a Circular Orbit 3.11 Effect of a Gravitational Moment on an Unsymmetric Gyrostat in a Circular Orbit Chapter 4 Complex Spacecraft 4.1 Generalized Active Forces 4.2 Potential Energy 4.3 Generalized Inertia Forces 4.4 Kinetic Energy CONTENTS V 4.5 Dynamical Equations 275 4.6 Linearized Dynamical Equations 277 4.7 Computerization of Symbol Manipulation 279 4.8 Discrete Multi-Degree-of-Freedom Systems 284 4.9 Lumped Mass Models of Spacecraft 296 4.10 Spacecraft with Continuous Elastic Components 318 4.11 Use of the Finite Element Method for the Construction of Modal Functions 332 Problem Sets 344 Problem Set 1 344 Problem Set 2 358 Problem Set 3 378 Problem Set 4 395 Appendixes 422 I Direction Cosines as Functions of Orientation Angles 422 II Kinematical Differential Equations in Terms Orientation Angles 427 Index 433

See more

The list of books you might like

Most books are stored in the elastic cloud where traffic is expensive. For this reason, we have a limit on daily download.