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Design of Guidance and Control Systems for Tactical Missiles

Qi Zaikang Lin Defu



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CRC Press
03 October 2019
Instruments & instrumentation engineering; Dynamics & vibration; Power generation & distribution; Automatic control engineering; Environmental science, engineering & technology
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.
By:   Qi Zaikang, Lin Defu
Imprint:   CRC Press
Country of Publication:   United Kingdom
Dimensions:   Height: 254mm,  Width: 178mm, 
Weight:   644g
ISBN:   9780367260415
ISBN 10:   0367260417
Pages:   240
Publication Date:   03 October 2019
Audience:   Professional and scholarly ,  Undergraduate
Format:   Hardback
Publisher's Status:   Active

Zaikang Qi Weapon Guidance and Control technology Chief Technical Expert. Serve as chair professor of Aircraft Guidance and Control Design in Beijing Institute of Technology, director of the institute of UAV Autonomous Control. Engaged in teaching and researching in the field of aircraft system design major for 60 years. Not only cultivated a batch of excellent young scholars and engineers, but also worked as chief engineer over several advanced researches and model scientific research projects. Member of the State Council Academic Degrees Committee Disciplinary Appraisal Team of the People's Republic of China; International editor of the American journal of Computers in mechanical engineering. Defu Lin Dr. Lin Defu received his Ph.D degree from Beijing Institute of Technology. Director of the institute of UAV Autonomous Control. He has more than 20 years' experience in the overall design and guidance and control of flight vehicles. He has worked as principle investigators for several key national projects. Due to his outstanding research work, he has been awarded second prize of National Scientific Invention and National Defense Science and Technology. He has more than 80 journal publications and serves as member of multiple academic committees.

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