Modern Missile Guidance - Rafael Yanushevsky

Modern Missile Guidance

Buch | Hardcover
240 Seiten
2007
Crc Press Inc (Verlag)
978-1-4200-6226-7 (ISBN)
255,60 inkl. MwSt
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Contains analytical results, that can be used for analysis and design of missile guidance and control systems. This book elucidates realistic guidance models that describe more precisely the dynamics of missile flight control systems and make the analytical results more effective in practice.
Written by an expert with more than 30 years of experience, Modern Missile Guidance contains new analytical results, obtained by the author, that can be used for analysis and design of missile guidance and control systems. This book covers not just new methods nor is it merely a compilation of older methods, although it includes both. The book discusses, in a logical progression, with its clear elucidation of the guidance laws, the entire field from missile dynamics to modeling and testing missile guidance and control systems.

In contrast to existing books that discuss very simple and often unrealistic guidance system models, this book presents missile guidance models that describe more precisely the dynamics of the missile flight control system, making analytical results more effective in practice. The analysis of missile guidance system models in the time-domain and in the frequency-domain allows the generation of different guidance laws that supplement each other.

Taking modern, rigorous approach that leads to improved performance in missile guidance applications, the book examines new guidance laws, and corresponding algorithms for generating and testing these laws, and includes effective new software programs developed by the author. The author provides an innovative presentation of the theoretical aspects of modern missile guidance that quite possibly cannot be found in any other book. It delineates new ideas that, once crystallized, will significantly improve missile systems performance.

Research & Technology Consulting, Bethesda, Maryland, USA

Basics of Missile Guidance. Parallel Navigation. Analysis of PN Guided Missile Systems in Time Domain. Analysis of PN Guided Missile Systems in Frequency Domain. Design of Guidance Laws Implementing Parallel Navigation: Time-Domain Approach. Design of Guidance Laws Implementing Parallel Navigation: Frequency-Domain Approach.
Guidance Law Performance Analysis Using Stochastic Inputs. Testing Guidance Laws Performance. Integrated Missile Design. Missile Guidance Software. Appendices.

Erscheint lt. Verlag 20.9.2007
Zusatzinfo 3 Tables, black and white; 1 Halftones, black and white; 72 Illustrations, black and white
Verlagsort Bosa Roca
Sprache englisch
Maße 178 x 254 mm
Gewicht 566 g
Themenwelt Technik Elektrotechnik / Energietechnik
Technik Umwelttechnik / Biotechnologie
ISBN-10 1-4200-6226-3 / 1420062263
ISBN-13 978-1-4200-6226-7 / 9781420062267
Zustand Neuware
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