Authors:
- Uses the sliding mode variable structure control method system to elaborate on single-aircraft and multi-body aircraft attitude setting and attitude control problems
- Proposes control laws to enhance the performance of spacecraft systems
- Suggests methods for meeting the many demands on spacecraft systems, such as strong disturbance rejection and high-precision control
Part of the book series: Advances in Industrial Control (AIC)
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Table of contents (18 chapters)
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Front Matter
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Preliminaries and Literature Review
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Front Matter
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Finite-Time Attitude Stabilization and Tracking Control of Spacecraft
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Front Matter
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Finite-Time Attitude Synchronization for Multiple Spacecraft
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Front Matter
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Finite-Time Formation Reconfiguration and Escorting Mission Based Coordination
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Front Matter
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About this book
As such, the book establishes a fundamental framework for these topics, while also highlighting the importance of integrated analysis. It is a useful resource for all researchers and students who are interested in this field, as well as engineers whose work involves designing flight vehicles.
Keywords
Authors and Affiliations
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School of Automation, Beijing Institute of Technology, Beijing, China
Yuanqing Xia, Jinhui Zhang
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Beijing Aerospace Automatic Control Institute, Beijing, China
Kunfeng Lu
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College of Computer and Information Sciences, Fujian Agriculture and Forestry University, Fuzhou, China
Ning Zhou
About the authors
Dr. Jinhui Zhang received his Ph.D. in Control Science and Engineering from the Beijing Institute of Technology, China in 2011. He is currently an associate professor at Tianjin University, China. From 2011 to 2016, he was an associate professor at Beijing University of Chemical Technology, China, and from 2010 to 2011, he was a research associate at the University of Hong Kong and the City University of Hong Kong. He has also worked as a visiting fellow at the University of Western Sydney, Australia. His research interests include networked control systems, robust control/filter theory, and disturbance rejection control.
Kunfeng Lu received his Ph.D. from the School of Automation, Beijing Institute of Technology, China in 2014. Currently, he works as an engineer at the Beijing Aerospace Automatic Control Institute (China) and the National Key Laboratory of Science and Technology on Aerospace Intelligent Control, China. His research interests include vehicle guidance and control, finite-time control, active disturbance rejection control, and sliding mode control.
Ning Zhou received her Ph.D. in Control Science and Engineering from the Beijing Institute of Technology, China in 2015. She is currently a postdoctoral researcher at the University of Groningen, the Netherlands, and a lecturer at the Research Institute of Big Data for Agriculture and Forestry, Fujian Agriculture and Forestry University, China. Her research interests include spacecraft attitude synchronization, sliding mode control, multi-agent control, and neural network control.
Bibliographic Information
Book Title: Finite Time and Cooperative Control of Flight Vehicles
Authors: Yuanqing Xia, Jinhui Zhang, Kunfeng Lu, Ning Zhou
Series Title: Advances in Industrial Control
DOI: https://doi.org/10.1007/978-981-13-1373-8
Publisher: Springer Singapore
eBook Packages: Intelligent Technologies and Robotics, Intelligent Technologies and Robotics (R0)
Copyright Information: Springer Nature Singapore Pte Ltd. 2019
Hardcover ISBN: 978-981-13-1372-1Published: 12 July 2018
Softcover ISBN: 978-981-13-4622-4Published: 19 January 2019
eBook ISBN: 978-981-13-1373-8Published: 02 July 2018
Series ISSN: 1430-9491
Series E-ISSN: 2193-1577
Edition Number: 1
Number of Pages: XXVI, 400
Number of Illustrations: 7 b/w illustrations, 162 illustrations in colour
Topics: Control and Systems Theory, Systems Theory, Control, Aerospace Technology and Astronautics, Complex Systems