Save 50% on book bundles
Immediately download your ebook while waiting for your print delivery. No promo code is needed.
Back to School Savings: Save up to 30% on print books and eBooks. No promo code needed.
Back to School Savings: Save up to 30%
Fast Satellite Attitude Maneuver and Control
1st Edition - August 2, 2022
Authors: Dong Ye, You Li, Yan Xiao
Paperback ISBN:
9 7 8 - 0 - 3 2 3 - 9 5 4 5 5 - 6
eBook ISBN:
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
Purchase Options
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, ChinaYL
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, ChinaYX
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