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Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods

Authors: Xie, Y., Chen, C., Liu, T., Wang, M.

  • Covers the key technologies of GNC system design for spacecraft rendezvous and docking  
  • Provides engineering tools that readers can apply to rendezvous and docking mission design  
  • Offers detailed step-by-step information on parameter design not covered elsewhere  
  • Presents sample simulations for each method, together with insightful explanations  
  • Includes the results of the Shenzhou spacecraft’s in-orbit flight mission  
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イーブック ¥17,159
価格の適用国: Japan (日本円価格は個人のお客様のみ有効) (小計)
  • イーブック版は、まもなく発売予定です。
  • 予定日: October 24, 2020
  • ISBN 978-981-15-6990-6
  • ウォーターマーク付、 DRMフリー
  • ファイル形式:
  • どの電子書籍リーダーからでもすぐにお読みいただけます。
ハードカバー ¥21,449
価格の適用国: Japan (日本円価格は個人のお客様のみ有効) (小計)
  • 予定日: October 24, 2020
  • ISBN 978-981-15-6989-0
  • 個人のお客様には、世界中どこでも配送料無料でお届けします。
  • Immediate ebook access, if available*, with your print order
この書籍について

This book focuses on the theory of and design methods for guidance, navigation, and control (GNC) in the context of spacecraft rendezvous and docking (RVD). The position and attitude dynamics and kinematics equations for RVD are presented systematically and in accordance with several different coordinate systems, including elliptical orbital frame, and recommendations are supplied on which of these equations to use in different phases of RVD. The book subsequently explains the basic principles and relative navigation algorithms of RVD sensors such as GNSS, radar, and camera-type RVD sensors. It also provides guidance algorithms and schemes for different phases of RVD, including the latest research advances in rapid RVD.  
In turn, the book presents a detailed introduction to intelligent adaptive control and proposes corresponding theoretical approaches to thruster configuration and control allocation for RVD. Emphasis is placed on the design method of active and passive trajectory protection in different phases of RVD, and on the safety design of the RVD mission as a whole. For purposes of verification, the Shenzhou spacecraft’s in-orbit flight mission is presented as well.  
All issues addressed are described and explained from basic principles to detailed engineering methods and examples, providing aerospace engineers and students both a basic understanding of, and numerous practical engineering methods for, GNC system design in RVD. 

著者について

Dr. Yongchun Xie is a Professor at Beijing Institute of Control Engineering (BICE). She received her Bachelor’s degree from Tsinghua University in 1989 and her Master’s degree and Ph.D. in Control Theory and Engineering from China Academy of Space Technology (CAST) in 1992 and 1994, respectively. From 1998 to 1999, she visited the Institute of Space and Astronautical Science in Japan as a senior scholar. She is currently a corresponding member of the IAA (International Academy of Astronautics) and has been engaged in the field of guidance, navigation, and control (GNC) for spacecraft rendezvous and docking (RVD) for nearly 20 years. She has participated in China’s manned space project as a leading engineer, responsible for the GNC systems design, and her GNC schemes have been successfully applied to RVD tasks for China’s spacecraft. Her research interests are chiefly in autonomous guidance and control of rendezvous and intelligent control of spacecraft. She has published more than 100 articles in technical journals and conference proceedings. 
Dr. Changqing Chen is a Senior Engineer at BICE. He obtained his Ph.D. in Control Theory and Engineering from CAST in 2008. He has been involved in rendezvous and docking guidance research since 2005, participated in the control scheme design of Shenzhou manned spacecraft, and was the main designer of the Tianzhou-1 cargo spacecraft control system. 
Dr. Tao Liu is a Senior Engineer at BICE. He obtained his Ph.D. in Control Theory and Engineering from CAST in 2010 and has been involved in China’s lunar exploration project. His current research interests include autonomous navigation in deep space exploration and guidance for rendezvous.
Dr. Min Wang is a Senior Engineer at BICE. She obtained her Ph.D. in Control Theory and Engineering from CAST in 2010 and subsequently began working there. She has participated in the GNC scheme design for the Shenzhou spacecraft and was the GNC system designer for the Tianzhou-1 cargo spacecraft. 

書籍の購入

イーブック ¥17,159
価格の適用国: Japan (日本円価格は個人のお客様のみ有効) (小計)
  • イーブック版は、まもなく発売予定です。
  • 予定日: October 24, 2020
  • ISBN 978-981-15-6990-6
  • ウォーターマーク付、 DRMフリー
  • ファイル形式:
  • どの電子書籍リーダーからでもすぐにお読みいただけます。
ハードカバー ¥21,449
価格の適用国: Japan (日本円価格は個人のお客様のみ有効) (小計)
  • 予定日: October 24, 2020
  • ISBN 978-981-15-6989-0
  • 個人のお客様には、世界中どこでも配送料無料でお届けします。
  • Immediate ebook access, if available*, with your print order
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書誌情報

Bibliographic Information
Book Title
Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods
Authors
Copyright
2021
Publisher
Springer Singapore
Copyright Holder
National Defense Industry Press
Distribution Rights
Distribution rights for print book in mainland China: National Defense Industry Press
イーブック ISBN
978-981-15-6990-6
DOI
10.1007/978-981-15-6990-6
ハードカバー ISBN
978-981-15-6989-0
Edition Number
1
Number of Pages
XII, 508
Number of Illustrations
49 b/w illustrations, 196 illustrations in colour
Topics

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