Dao dan kong zhi he zhi dao de fei xian xing she ji fang fa = Nonlinear design approaches for missile control and guidance  Nonlinear Design Approaches for Missile Control and Guidance 

• Product Details

  Product #

  2007145B

  Author(s)

  Zhang, You'an

  City

  Beijing 

  Country

  China 

  Language

  Chinese (simplified) 

  ISBN

  9787118031652 

  Date of Publication

  2003 

  Publisher

  Guo fang gong ye chu ban she  

  Cover Type

  Soft cover 

  Pages

  177 

  Subject

  Military and Naval

   

• Product Details in Original Language

  Author

  张友安

  Publisher

  国防工业出版社  

• Description

  Nonlinear Design Approaches for Missile Control and Guidance Zhang Youan, a professor at the School of Automation at Beijing Institute of Technology, has long been engaged in research in the field of missile control and guidance. He is not only highly regarded in academia, but has also participated in numerous major national scientific research projects, making significant contributions to the development of China's missile technology. His monograph, "Nonlinear Design Methods for Missile Control and Guidance," embodies his many years of research and is an authoritative work in the field. This work details the theory and applications of nonlinear design in missile control and guidance systems. It not only covers the fundamentals of classical control theory but also delves into the application of modern nonlinear control techniques in missile systems. From mathematical modeling and controller design to simulation verification, it comprehensively demonstrates the importance of nonlinear design methods in missile control and guidance. This book is not only suitable for researchers and engineers in the field of missile technology, but also serves as an excellent introductory textbook for students and enthusiasts interested in missile control and guidance. Its in-depth and accessible content, combining theoretical analysis with practical examples, will help readers better understand and master the nonlinear design methods used in missile control and guidance.