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.
1. Fast Satellite Attitude Maneuver and Control - p. iii 2. Cover - p. iii 3. Title Page - p. iii 4. Copyright Page - p. iv 5. Table of Contents - p. iv 6. Preface - p. xi 7. Acknowledgments - p. xv 8. Chapter 1 Overview - p. 1 9. Chapter 2 Mathematical model and basic control theory - p. 29 10. Chapter 3 Near time-optimal control based on analytical trajectory planning - p. 43 11. Chapter 4 Time-efficient robust PID plus control with constraints - p. 75 12. Chapter 5 Bang–bang logic-based time-efficient sliding mode control - p. 97 13. Chapter 6 Robust finite-time control based on three-stage structure-sliding mode - p. 121 14. Chapter 7 Finite-time output feedback attitude control - p. 147 15. Chapter 8 Observer-based continuous finite-time attitude control - p. 161 16. Chapter 9 Neural network-based finite-time fault-tolerant attitude control - p. 181 17. Chapter 10 Hybrid thrusters and reaction wheel-based attitude control - p. 201 18. Chapter 11 Finite-time attitude control with hybrid actuators - p. 215 19. Chapter 12 A control allocation approach for hybrid actuators - p. 233 20. Chapter 13 Conclusions and future works - p. 253 21. Index - p. 257
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.
1. Fast Satellite Attitude Maneuver and Control - p. iii 2. Cover - p. iii 3. Title Page - p. iii 4. Copyright Page - p. iv 5. Table of Contents - p. iv 6. Preface - p. xi 7. Acknowledgments - p. xv 8. Chapter 1 Overview - p. 1 9. Chapter 2 Mathematical model and basic control theory - p. 29 10. Chapter 3 Near time-optimal control based on analytical trajectory planning - p. 43 11. Chapter 4 Time-efficient robust PID plus control with constraints - p. 75 12. Chapter 5 Bang–bang logic-based time-efficient sliding mode control - p. 97 13. Chapter 6 Robust finite-time control based on three-stage structure-sliding mode - p. 121 14. Chapter 7 Finite-time output feedback attitude control - p. 147 15. Chapter 8 Observer-based continuous finite-time attitude control - p. 161 16. Chapter 9 Neural network-based finite-time fault-tolerant attitude control - p. 181 17. Chapter 10 Hybrid thrusters and reaction wheel-based attitude control - p. 201 18. Chapter 11 Finite-time attitude control with hybrid actuators - p. 215 19. Chapter 12 A control allocation approach for hybrid actuators - p. 233 20. Chapter 13 Conclusions and future works - p. 253 21. Index - p. 257
