Adaptive Predefined-Time Attitude Control for Spacecraft presents the latest advancements in spacecraft control dynamics, with a particular focus on time-bound strategies that guarantee rapid and smooth system stabilization under realistic mission constraints. Rooted in the expertise of scholars with extensive experience in nonlinear and adaptive control, the book establishes a solid theoretical foundation in finite-time and predefined-time formulations before transitioning to sophisticated techniques such as fuzzy logic, dynamic surface control, neural networks, and event-triggered design. Subsequent chapters broaden the scope to encompass multi-spacecraft coordination and time-triggered adaptation, reflecting the growing trend toward autonomy and intelligent systems in modern aerospace applications.
Readers are guided through a cohesive suite of state-of-the-art methodologies, along with insights into emerging trends and future frontiers, all engineered to optimize reliability, efficiency, and fault tolerance. Graduate students, early-career researchers, and experienced engineers in both academia and industry will find this volume a comprehensive and indispensable reference for the design and deployment of intelligent attitude control systems in modern flight and satellite missions.
1. 1: Introduction - p. 3 2. 2: Mathematical model of rigid spacecraft - p. 7 3. Part Two: Finite-time attitude control of rigid spacecraft - p. P2 4. 3: Neural-network-based adaptive finite-time output constraint control for rigid spacecraft - p. 17 5. 4: Finite-time command-filtered approximation-free attitude tracking control of rigid spacecraft - p. 41 6. Part Three: Fixed-time sliding mode attitude control of rigid spacecraft - p. P3 7. 5: Adaptive fixed-time control for rigid spacecraft using a double power reaching law - p. 67 8. 6: Adaptive nonsingular fixed-time attitude stabilization of uncertain spacecraft - p. 91 9. 7: Neural-network-based adaptive singularity-free fixed-time attitude tracking control for spacecraft - p. 123 10. Part Four: Predefined-time backstepping attitude control of rigid spacecraft - p. P4 11. 8: Adaptive nonsingular predefined-time control for attitude stabilization of rigid spacecraft - p. 159 12. 9: Predefined-time disturbance estimation and attitude control for rigid spacecraft - p. 175 13. 10: Predefined-time approximation-free attitude constraint control of rigid spacecraft - p. 189 14. Part Five: Predefined-time dynamic surface attitude control of rigid spacecraft - p. P5 15. 11: Adaptive fuzzy predefined-time dynamic surface control for attitude tracking of spacecraft with state constraints - p. 215 16. 12: Adaptive predefined-time event-triggered control for attitude consensus of multiple spacecraft with time-varying state constraints - p. 243 17. Subject index - p. 271
Adaptive Predefined-Time Attitude Control for Spacecraft presents the latest advancements in spacecraft control dynamics, with a particular focus on time-bound strategies that guarantee rapid and smooth system stabilization under realistic mission constraints. Rooted in the expertise of scholars with extensive experience in nonlinear and adaptive control, the book establishes a solid theoretical foundation in finite-time and predefined-time formulations before transitioning to sophisticated techniques such as fuzzy logic, dynamic surface control, neural networks, and event-triggered design. Subsequent chapters broaden the scope to encompass multi-spacecraft coordination and time-triggered adaptation, reflecting the growing trend toward autonomy and intelligent systems in modern aerospace applications.
Readers are guided through a cohesive suite of state-of-the-art methodologies, along with insights into emerging trends and future frontiers, all engineered to optimize reliability, efficiency, and fault tolerance. Graduate students, early-career researchers, and experienced engineers in both academia and industry will find this volume a comprehensive and indispensable reference for the design and deployment of intelligent attitude control systems in modern flight and satellite missions.
1. 1: Introduction - p. 3 2. 2: Mathematical model of rigid spacecraft - p. 7 3. Part Two: Finite-time attitude control of rigid spacecraft - p. P2 4. 3: Neural-network-based adaptive finite-time output constraint control for rigid spacecraft - p. 17 5. 4: Finite-time command-filtered approximation-free attitude tracking control of rigid spacecraft - p. 41 6. Part Three: Fixed-time sliding mode attitude control of rigid spacecraft - p. P3 7. 5: Adaptive fixed-time control for rigid spacecraft using a double power reaching law - p. 67 8. 6: Adaptive nonsingular fixed-time attitude stabilization of uncertain spacecraft - p. 91 9. 7: Neural-network-based adaptive singularity-free fixed-time attitude tracking control for spacecraft - p. 123 10. Part Four: Predefined-time backstepping attitude control of rigid spacecraft - p. P4 11. 8: Adaptive nonsingular predefined-time control for attitude stabilization of rigid spacecraft - p. 159 12. 9: Predefined-time disturbance estimation and attitude control for rigid spacecraft - p. 175 13. 10: Predefined-time approximation-free attitude constraint control of rigid spacecraft - p. 189 14. Part Five: Predefined-time dynamic surface attitude control of rigid spacecraft - p. P5 15. 11: Adaptive fuzzy predefined-time dynamic surface control for attitude tracking of spacecraft with state constraints - p. 215 16. 12: Adaptive predefined-time event-triggered control for attitude consensus of multiple spacecraft with time-varying state constraints - p. 243 17. Subject index - p. 271
