The Motion Control System of the Legendary Scud-B Missile Description and Mathematical Analysis By: Bodo E. Seyfert This book provides the historical background that led to the development of the SCUD-B operational-tactical missile. For more than fifty years, it was the most widely deployed missile. The systems are subjected to a thorough mathematical analysis performed on the electronic element level. The analysis results are confirmed by replicating the required hardware tests in the MATHCAD and MATLAB/SIMULINK environments, thus allowing the author to obtain motion stabilization and range control algorithms. The information provided in this book is based upon original Soviet literature declassified in the late 1980s and upon a wide range of articles concerned with the development of the R-17/R-17M missile, which were published after the breakdown of the former Soviet Union.

The Scud missile was developed as the centerpiece of Soviet plans to fight nuclear war in the heart of Europe. However, it was never used in its intended role and has instead become a symbol of the changing nature of warfare in the aftermath of the Cold War. Saddam Hussein's Iraqi armed forces were almost helpless in the face of the Coalition forces in the 1991 Gulf War; the only weapon that Iraq could use to injure the Coalition forces was its arsenal of Scud missiles. This book explores the development and variants of the missile and its launch systems, its proliferation outside of the West, and its role in conflicts around the world.

Airborne Vehicle Guidance and Control Systems is a broad and wide- angled engineering and technological area for research, and continues to be important not only in military defense systems but also in industrial process control and in commercial transportation networks such as various Global Positioning Systems (GPS). The book fills a long-standing gap in the literature. The author is retired from the Air Force Institute and received the Air Force's Outstanding Civilian Career Service Award.

Design of Guidance and Control Systems for Tactical Missiles presents a modern, comprehensive study of the latest design methods for tactical missile guidance and control. It analyzes autopilot designs, seeker system designs, guidance laws and theories, and the internal and external disturbances affecting the performance factors of missile guidance control systems. The text combines detailed examination of key theories with practical coverage of methods for advanced missile guidance control systems. It is valuable content for professors and graduate-level students in missile guidance and control, as well as engineers and researchers who work in the area of tactical missile guidance and control.