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| Advances in Missile Guidance Theory |
Joseph Ben-Asher, Israel Military Industries
Isaac Yaesh, Israel Military Industries
Progress in Astronautics and Aeronautics Series, V-180
Published by AIAA, © 1998, 200 pages, Mixed media
ISBN-10: 1-56347-275-9
ISBN-13: 978-1-56347-275-6
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AIAA Member Price:
$79.95
List Price:
$104.95
AIAA Members Save 24%!
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This book is about terminal guidance of intercepting missiles. It contains a variety of newly developed guidance methods based on linear quadratic optimization problems. This application-oriented book employs widely used and thoroughly developed theories such as LQ and H-infinity to missile guidance. Numerous examples help the reader to gain greater understanding of the relative merits and shortcomings of the various methods. Both the analytical derivations and the numerical computations of the examples are carried out by MAPLE and MATLAB® subroutines. The codes are provided with the book.
MATLAB is a registered trademark of The MathWorks, Inc.
About the Author:
Ben-Asher has left Israel Military Industries and is now with Wales Ltd. Yaesh’s new e-mail address is izi@inter.net.il
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Table of Contents:
- Introduction
- Mathematical Background
- Optimal Guidance Based on Linear-Quadratic One-Sided Optimization
- Optimal Guidance Based on Linear-Quadratic Differential Games
- Optimal Guidance with Reduced Sensitivity to Time-to-Go Estimation Errors
- Robust Guidance Methods
- Optimal Guidance with Multiple Targets
- Appendix A—Justification of the Sweep Assumption
- Appendix B—Mathematical Computations with MAPLE
- Appendix C—Numerical Computations with MATLAB
- Index
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