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Applied Min-Max Approach to Missile Guidance and Control

Applied Min-Max Approach to Missile Guidance and Control - Progress in Astronautics and Aeronautics

Hardback (30 May 2005)

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Publisher's Synopsis

This book is concerned with robust control and uses a min-max approach or a worst-case design with respect to a specific cost. The book consists of two parts. The first part is theoretical and summarizes the author's research in control of linear systems. The second part is practical and addresses guidance and control of missiles with emphasis on minimum and non-minimum phase systems. The significant contribution of the first part is the systematic development of the author's ""pole clustering"" and ""differential game"" research (MIN-MAX). The second part addresses missile guidance and control on a somewhat tutorial basis and provides interesting insight into the behavior of tail vs. Canard controlled missiles.

Book information

ISBN: 9781563476952
Publisher: American Institute of Aeronautics & Astronautics
Imprint: AIAA
Pub date:
DEWEY: 629.8312
DEWEY edition: 22
Language: English
Number of pages: 298
Weight: 598g
Height: 228mm
Width: 152mm
Spine width: 19mm