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Fast Satellite Attitude Maneuver and Control
1st Edition - August 2, 2022
Authors: Dong Ye, You Li, Yan Xiao
Paperback ISBN:9780323954556
9 7 8 - 0 - 3 2 3 - 9 5 4 5 5 - 6
eBook ISBN:9780323954563
9 7 8 - 0 - 3 2 3 - 9 5 4 5 6 - 3
Fast Satellite Attitude Maneuver and Control introduces the concept of agile satellites and corresponding fast maneuver attitude control systems, systematically and… Read more
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Fast Satellite Attitude Maneuver and Control introduces the concept of agile satellites and corresponding fast maneuver attitude control systems, systematically and comprehensively presenting recent research results of fast maneuver attitude control for agile satellites by using advanced nonlinear control techniques. This reference book focuses on modeling and attitude control, considering different actuator combinations, actuator installation deviation, actuator fault, and flexible appendage coupling effect for agile satellites. The book provides a unified platform for understanding and applicability of agile satellites fast maneuverer and stabilization control for different purposes.
It will be an excellent resource for researchers working on spacecraft design, nonlinear control systems, vehicle systems and complex control systems.
Unifies existing and emerging concepts concerning nonlinear control theory, fault tolerant, and attitude control for agile satellites
Provides a series of the latest results, including, but not limited to, fast maneuverer and stabilization control, hybrid actuator control, nonlinear attitude control, fault tolerant control, and active vibration suppression towards agile satellites
Comprehensively captures recent advances of theory, technological aspects and applications of fast maneuverer and stabilization control in agile satellites
Addresses research problems in each chapter, along with numerical and simulation results that reflect engineering practice and demonstrate the focus of developed analysis and synthesis approaches
Contains comprehensive, up-to-date references, which play an indicative role for further study
Cover
Title page
Table of Contents
Copyright
Preface
Acknowledgments
Chapter 1: Overview
Abstract
1.1: Introduction
1.2: Development status and trend of agile satellite
1.3: Research status of optimal attitude trajectory planning
1.4: Research status of large-angle maneuver attitude control algorithm
1.5: Research status of hybrid control
References
Part I: Preliminaries
Chapter 2: Mathematical model and basic control theory
Abstract
2.1: Spacecraft kinetic model and satellite parameters
2.2: Spacecraft dynamic model
2.3: Relevant control theory
Part II: Research on attitude control methods for fast maneuver satellites
Chapter 3: Near time-optimal control based on analytical trajectory planning
Abstract
3.1: Introduction
3.2: Problem formulation
3.3: Controller design
3.4: Simulation results
3.5: Conclusion
References
Chapter 4: Time-efficient robust PID plus control with constraints
Abstract
4.1: Introduction
4.2: Time-efficient PID plus controller
4.3: Angular velocity and control torque constraint
4.4: Simulation results
4.5: Conclusion
References
Chapter 5: Bang–bang logic-based time-efficient sliding mode control
Abstract
5.1: Introduction
5.2: Time-efficient sliding mode controller
5.3: Simulation results
5.4: Conclusion
References
Chapter 6: Robust finite-time control based on three-stage structure-sliding mode
Abstract
6.1: Introduction
6.2: Finite-time controller for attitude stabilization control
6.3: Finite-time controller for attitude tracking control
6.4: Simulation results
6.5: Conclusion
References
Part III: Research on finite time attitude control for fast maneuver rigid-flexible coupling satellites
Chapter 7: Finite-time output feedback attitude control
Abstract
7.1: Introduction
7.2: Main results
7.3: Simulation results
7.4: Conclusion
References
Chapter 8: Observer-based continuous finite-time attitude control
Abstract
8.1: Introduction
8.2: Continuous terminal sliding mode control based on ESO
8.3: Simulation results
8.4: Conclusion
References
Chapter 9: Neural network-based finite-time fault-tolerant attitude control
Abstract
9.1: Introduction
9.2: Problem formulation
9.3: LeNN-based finite time fault-tolerant controller design
9.4: Simulation results
9.5: Conclusion
References
Part IV: Hybrid actuator-based fast maneuver and stabilization control for rigid satellites
Chapter 10: Hybrid thrusters and reaction wheel-based attitude control
Abstract
10.1: Introduction
10.2: Problem formulation
10.3: Hybrid tracking controller design
10.4: Simulation results
10.5: Conclusion
References
Chapter 11: Finite-time attitude control with hybrid actuators
Abstract
11.1: Introduction
11.2: Problem formulation
11.3: Design of controllers
11.4: Simulation results
11.5: Conclusion
References
Chapter 12: A control allocation approach for hybrid actuators
Abstract
12.1: Introduction
12.2: Problem formulation
12.3: Control torque allocation considering singularity of CMGs
12.4: Simulation results
12.5: Conclusion
References
Chapter 13: Conclusions and future works
Abstract
13.1: General conclusion
13.2: Future work
Index
No. of pages: 278
Language: English
Published: August 2, 2022
Imprint: Academic Press
Paperback ISBN: 9780323954556
eBook ISBN: 9780323954563
DY
Dong Ye
Dong Ye is a Professor at the School of Astronautics, Harbin Institute, in China. His research interests include spacecraft dynamics and control and hardware-in-the-loop simulation technique.
Affiliations and expertise
Professor, School of Astronautics, Harbin Institute, China
YL
You Li
You Li graduated from Harbin Institute of Technology in 2017, and now is a Lecturer at the School of Aerospace Science and Technology, Xidian University, in China. His work is mainly focusing on satellite attitude control, especially on satellite attitude fast maneuver.
Affiliations and expertise
Lecturer, School of Aerospace Science and Technology, Xidian University, China
YX
Yan Xiao
Yan Xiao received his Ph.D. degree in Aeronautical and Astronautical Science and Technology from the Harbin Institute of Technology (HIT) and now is an Assistant Professor at the School of Astronautics, HIT. His current research interests include nonlinear control, spacecraft attitude dynamics and control, coordination control, etc.
Affiliations and expertise
Assistant Professor, School of Astronautics, HIT, China