Spacecraft Electromagnetic Docking and Separation
Elsevier (Publisher)
Will be published approx. on 1. September 2026
Book
Paperback/Softback
400 pages
978-0-443-49334-8 (ISBN)
Description
Spacecraft Electromagnetic Docking and Separation solves problems for spacecraft electromagnetic docking and separation control system using different control methods: instead of the widely used proportional-integral-derivative controller or PID control. The book focuses on presenting a variety of control strategies tailored for spacecraft electromagnetic docking and separation, accompanied by stability proofs that integrate Lyapunov stability theory with sliding mode theory, LMIs-based theorems, model predictive control theories, reinforcement study theories and other frameworks, so the reader can understand how to handle different kinds of disturbances and perturbations in actual orbiting spacecraft. The book also provides a review of magnetic field, magnetic field force model (both the near-field model and the far-field model), useful lemmas and dynamic modelling methods of spacecraft relative motion, which can serve as first stage analysis for further research and are especially important in the initial design phase of a spacecraft electromagnetic docking and separation control system
More details
Language
English
Place of publication
Philadelphia
United States
Target group
Professional and scholarly
Product notice
Paperback (trade)
Unsewn / adhesive bound
Dimensions
Height: 229 mm
Width: 152 mm
Weight
450 gr
ISBN-13
978-0-443-49334-8 (9780443493348)
Copyright in bibliographic data is held by Nielsen Book Services Limited or its licensors: all rights reserved.
Schweitzer Classification
Persons
Keke Shi is an Associate Professor at Xi'an University of Science and Technology, China. Dr Shi's research interests include spacecraft electromagnetic docking and separation
Chuang Liu is an Associate Professor at Northwestern Polytechnical University, China. He is also Scientific Committee Member of Aeromeet 2022. He received the COSPAR Outstanding Paper Award for Young Scientists in 2020. His research focuses on aerospace engineering. Xiaokui Yue is a Professor at Northwestern Technical University, China. His research has focused on the frontiers of space exploration and on computational methods for nonlinear dynamical systems. Mahe Shu is a PhD research student at Northwestern Polytechnical University. Research interests include spacecraft electromagnetic docking and separation
Chuang Liu is an Associate Professor at Northwestern Polytechnical University, China. He is also Scientific Committee Member of Aeromeet 2022. He received the COSPAR Outstanding Paper Award for Young Scientists in 2020. His research focuses on aerospace engineering. Xiaokui Yue is a Professor at Northwestern Technical University, China. His research has focused on the frontiers of space exploration and on computational methods for nonlinear dynamical systems. Mahe Shu is a PhD research student at Northwestern Polytechnical University. Research interests include spacecraft electromagnetic docking and separation
Author
Xi'an University of Science and Technology, China
Associate Professor, Northwestern Polytechnical University, China
Professor, Northwestern Technical University, China
Northwestern Polytechnical University, China
Content
1. Introduction of basic knowledge
2. Coupled Orbit-Attitude Tracking Control for Spacecraft Electromagnetic Docking
3. Intermediate Observer-based Control for Spacecraft Electromagnetic Docking
4. Active Disturbance Rejection Control for Spacecraft Electromagnetic Docking
5. Disturbance Observer-based Control for Spacecraft Electromagnetic Docking
6. Model Predictive Control for Spacecraft Electromagnetic Docking
7. Deep Reinforcement Learning-based Control for Spacecraft Electromagnetic Docking
8. Sliding Mode Tracking Control for Spacecraft Electromagnetic Separation
9. Optimizations-based Impedance Control for Spacecraft Electromagnetic Separation
10. Integrated Control for Spacecraft Electromagnetic Docking and Separation
2. Coupled Orbit-Attitude Tracking Control for Spacecraft Electromagnetic Docking
3. Intermediate Observer-based Control for Spacecraft Electromagnetic Docking
4. Active Disturbance Rejection Control for Spacecraft Electromagnetic Docking
5. Disturbance Observer-based Control for Spacecraft Electromagnetic Docking
6. Model Predictive Control for Spacecraft Electromagnetic Docking
7. Deep Reinforcement Learning-based Control for Spacecraft Electromagnetic Docking
8. Sliding Mode Tracking Control for Spacecraft Electromagnetic Separation
9. Optimizations-based Impedance Control for Spacecraft Electromagnetic Separation
10. Integrated Control for Spacecraft Electromagnetic Docking and Separation