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Adaptive Predefined-Time Attitude Control for Spacecraft: Aerospace Engineering

Autor Qiang Chen, Shuzong Xie, Xiongxiong He, Shubo Wang
en Limba Engleză Paperback – oct 2026
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.


  • 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


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