Overview
- Provides readers with detailed concepts and design methods for spacecraft dynamics and control
- Summarizes practical spacecraft applications of control theories and methods in China
- Serves as a guide for follow-up engineering development and research on control theory and methods
Part of the book series: Space Science and Technologies (SST)
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Table of contents (7 chapters)
Keywords
- Spacecraft Attitude Determination
- Attitude Sensors Error Modelling
- Geometric Attitude Determination
- State Estimation Attitude Determination
- Attitude Sensors Relative Error Calibration
- High Accuracy Attitude Calibration of Ground Afterwards
- Imaging Drift Angle Determination
- Space Attitude Control
- Thruster Based Attitude Control
- Angular Momentum Management Based Attitude Control
- Angular Momentum Management Manipulation Strategy
- Liquid-filled Spacecraft Control
- Multi-body Spacecraft Attitude Control
- Spacecraft Autonomous Navigation, Guidance, and Control
- Absolute Autonomous Navigation
- Relative Autonomous Navigation
- Rendezvous and Docking Guidance and Control
- Reentry Guidance and Control
- Soft Landing of Extraterrestrial Objects Guidance and Control
- Interstellar Flight Guidance and Control
About this book
Authors and Affiliations
About the authors
Professor Yongjun Lei is currently a senior chief designer of spacecraft control systems at Beijing Institute of Control Engineering. He has been engaged in the control scheme design for high- performance low-orbit satellites. His research interests include modeling and control of complicated systems, such as flexible structures and multi-body spacecraft. He has won six ministerial level prizes (first class once, second class three times, and third class twice).
Professor Jianxin Guo is a director designer of medium- and high-orbit satellite control systems at Beijing Institute of Control Engineering. He has been engaged in the control scheme design for the BEIDOU navigation satellite system and a new generation communication satellites of China. His current research interests include spacecraft orbit control and multi-body spacecraft complex control. He has won four ministerial level prizes (first class three times and second class once).
Bin Meng is Professor at the Beijing Institute of Control Engineering, where she was a postdoctoral fellow from 2005 to 2007. She received her Ph.D. degree in control theory and application fromthe Chinese Academy of Sciences in 2005. From 2016 to 2017, she was Visiting Academic at the University of Leeds, UK. Her majors are spacecraft guidance and control, and adaptive control theory and applications. As Principle Investigator or Co-investigator, she has led or been involved in more than 10 research projects. She has published more than 30 research articles and 5 book chapters and has been granted 5 patents. She has won various awards, such as the 2nd prize of the 2013 National Technological Invention Award.
Bibliographic Information
Book Title: Spacecraft Dynamics and Control
Authors: Yongchun Xie, Yongjun Lei, Jianxin Guo, Bin Meng
Series Title: Space Science and Technologies
DOI: https://doi.org/10.1007/978-981-33-6448-6
Publisher: Springer Singapore
eBook Packages: Engineering, Engineering (R0)
Copyright Information: Beijing Institute of Technology Press 2022
Hardcover ISBN: 978-981-33-6447-9Published: 14 July 2021
Softcover ISBN: 978-981-33-6450-9Published: 15 July 2022
eBook ISBN: 978-981-33-6448-6Published: 13 July 2021
Series ISSN: 2730-6410
Series E-ISSN: 2730-6429
Edition Number: 1
Number of Pages: XIV, 422
Number of Illustrations: 82 b/w illustrations, 110 illustrations in colour
Topics: Vibration, Dynamical Systems, Control, Aerospace Technology and Astronautics, Control and Systems Theory