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Advances in Missile Guidance Theory

Hardcover
$104.95
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Pub Date: January 1, 1998

Dewey: 623.4519

LCCN: 98194778

Lexile Code: 0000

Target Age Group: NA to NA

Physical Info: 0.71" H x 9.16" L x 6.46" W ( 1.10 lbs) 200 pages

Series: Progress in Astronautics and Aeronautics

Descriptions, Reviews, etc.

Description: 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.

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