Adaptive Predefined-Time Attitude Control for Spacecraft: Aerospace Engineering
Autor Qiang Chen, Shuzong Xie, Xiongxiong He, Shubo Wangen Limba Engleză Paperback – oct 2026
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.
- Enhances overall spacecraft performance through intelligent control strategies such as neural networks and finite-time control, ensuring robust operation in highly complex and uncertain environments
- Delivers precise and reliable attitude stabilization using advanced techniques like fixed-time sliding mode control and predefined-time backstepping, maintaining accuracy even in the presence of dynamic external disturbances
- Ensures fault resilience and mission continuity by employing adaptive and event-triggered control methods that respond proactively to unexpected system failures, preserving functionality without compromising performance
- Promotes control efficiency and autonomy by integrating real-time decision-making frameworks and low-complexity algorithms that enable spacecraft to adapt to evolving mission conditions with minimal ground intervention
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Specificații
ISBN-13: 9780443447778
ISBN-10: 0443447772
Pagini: 630
Dimensiuni: 152 x 229 mm
Editura: ELSEVIER SCIENCE
Seria Aerospace Engineering
ISBN-10: 0443447772
Pagini: 630
Dimensiuni: 152 x 229 mm
Editura: ELSEVIER SCIENCE
Seria Aerospace Engineering
Cuprins
Part I: Fundamentals and mathematical modeling
1. Introduction
2. Mathematical model of rigid spacecraft
Part II: Finite-time attitude control of rigid spacecraft
3. Neural-network-based adaptive finite-time output constraint control for rigid spacecraft
4. Finite-time command-filtered approximation-free attitude tracking control of rigid spacecraft
Part III: Fixed-time sliding mode attitude control of rigid spacecraft
5. Adaptive fixed-time control for rigid spacecraft using a double power reaching law
6. Adaptive nonsingular fixed-time attitude stabilization of uncertain spacecraft
7. Neural-network-based adaptive singularity-free fixed-time attitude tracking control for
spacecraft
Part IV: Predefined-time backstepping attitude control of rigid spacecraft
8. Adaptive nonsingular predefined-time control for attitude stabilization of rigid spacecraft
9. Predefined-time disturbance estimation and attitude control for rigid spacecraft
10. Predefined-time approximation-free attitude constraint control of rigid spacecraft
Part V: Predefined-time dynamic surface attitude control of rigid spacecraft
11. Adaptive fuzzy predefined-time dynamic surface control for attitude tracking of spacecraft with state constraints
12 Adaptive predefined-time event-triggered control for attitude consensus of multiple spacecraft with time-varying state constraints
1. Introduction
2. Mathematical model of rigid spacecraft
Part II: Finite-time attitude control of rigid spacecraft
3. Neural-network-based adaptive finite-time output constraint control for rigid spacecraft
4. Finite-time command-filtered approximation-free attitude tracking control of rigid spacecraft
Part III: Fixed-time sliding mode attitude control of rigid spacecraft
5. Adaptive fixed-time control for rigid spacecraft using a double power reaching law
6. Adaptive nonsingular fixed-time attitude stabilization of uncertain spacecraft
7. Neural-network-based adaptive singularity-free fixed-time attitude tracking control for
spacecraft
Part IV: Predefined-time backstepping attitude control of rigid spacecraft
8. Adaptive nonsingular predefined-time control for attitude stabilization of rigid spacecraft
9. Predefined-time disturbance estimation and attitude control for rigid spacecraft
10. Predefined-time approximation-free attitude constraint control of rigid spacecraft
Part V: Predefined-time dynamic surface attitude control of rigid spacecraft
11. Adaptive fuzzy predefined-time dynamic surface control for attitude tracking of spacecraft with state constraints
12 Adaptive predefined-time event-triggered control for attitude consensus of multiple spacecraft with time-varying state constraints