Optimal Spacecraft Rotational Maneuvers ( Volume 3 )

Publication series :Volume 3

Author: Junkins   J. L.;Turner   J. D.  

Publisher: Elsevier Science‎

Publication year: 2012

E-ISBN: 9780444600318

P-ISBN(Paperback): 9780444426192

P-ISBN(Hardback):  9780444426192

Subject: V412 flight mechanics

Language: ENG

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Description

This monograph has grown out of the authors' recent work directed toward solving a family of problems which arise in maneuvering modern spacecraft. The work ranges from fundamental developments in analytical dynamics and optimal control to a significant collection of example applications. The primary emphasis herein is upon the most central analytical and numerical methods for determining optimal rotational maneuvers of spacecraft. The authors focus especially upon the large angle nonlinear maneuvers, and also consider large rotational maneuvers of flexible vehicles with simultaneous vibration suppression/arrest. Each chapter includes a list of references.

The book provides much new material which will be of great interest to practising professionals and advanced graduate students working in the general areas of spacecraft technology, applied mathematics, optimal control theory, and numerical optimization. Chapter 11 in particular presents new information that will be found widely useful for terminal control and tracking maneuvers.

Chapter

Front Cover

pp.:  1 – 4

Copyright Page

pp.:  5 – 10

PREFACE

pp.:  6 – 20

Table of Contents

pp.:  10 – 6

CHAPTER 1. INTRODUCTION

pp.:  20 – 24

CHAPTER 3. BASIC PRINCIPLES OF DYNAMICS

pp.:  60 – 100

CHAPTER 4. ROTATIONAL DYNAMICS OF RIGID AND MULTIPLE RIGID BODY SPACECRAFT

pp.:  100 – 153

CHAPTER 5. DYNAMICS OF FLEXIBLE SPACECRAFT

pp.:  153 – 190

CHAPTER 6. ELEMENTS OF OPTIMAL CONTROL THEORY

pp.:  190 – 243

CHAPTER 7. NUMERICAL SOLUTION OF TWO POINT BOUNDARY VALUE PROBLEMS

pp.:  243 – 269

CHAPTER 8. OPTIMAL MANEUVERS OF RIGID SPACECRAFT

pp.:  269 – 328

CHAPTER 9. OPTIMAL LARGE-ANGLE SINGLE-AXIS MANEUVERS OF FLEXIBLE SPACECRAFT

pp.:  328 – 377

CHAPTER 10. FREQUENCY-SHAPED LARGE-ANGLE MANEUVERS OF FLEXIBLE SPACECRAFT

pp.:  377 – 423

CHAPTER 11. COMPUTATIONAL METHODS FOR CLOSED - LOOP CONTROL PROBLEMS

pp.:  423 – 475

APPENDIX A: AUTONOMOUS SYSTEMS OF ORDINARY DIFFERENTIAL EQUATIONS

pp.:  475 – 506

APPENDIX Β: CLOSED-FORM SOLUTION FOR AN INTEGRAL CONTAINING MATRIX EXPONENTIALS

pp.:  506 – 509

APPENDIX C: CLOSED-FORM SOLUTIONS FOR CONVOLUTION MATRIX INTEGRALS AND SENSITIVITY CALCULATIONS

pp.:  509 – 520

APPENDIX D: ANALYTICAL SOLUTION OF THE TWO BODY PROBLEM (KEPLERIAN MOTION)

pp.:  520 – 522

APPENDIX E: AN ANALYTIC FOURIER TRANSORM FOR A CLASS OF FINITE-TIME CONTROL PROBLEMS

pp.:  522 – 529

INDEX

pp.:  529 – 535

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