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Fault-Tolerant Attitude Control of Spacecraft

Autor Qinglei Hu, Bing Xiao, Bo Li, Youmin Zhang
en Limba Engleză Paperback – 18 iun 2021
Fault-Tolerant Attitude Control of Spacecraft presents the fundamentals of spacecraft fault-tolerant attitude control systems, along with the most recent research and advanced, nonlinear control techniques. This book gives researchers a self-contained guide to the complex tasks of envisaging, designing, implementing and experimenting by presenting designs for integrated modeling, dynamics, fault-tolerant attitude control, and fault reconstruction for spacecraft. Specifically, the book gives a full literature review and presents preliminaries and mathematical models, robust fault-tolerant attitude control, fault-tolerant attitude control with actuator saturation, velocity-free fault tolerant attitude control, finite-time fault-tolerant attitude tracking control, and active fault-tolerant attitude contour.
Finally, the book looks at the future of this interesting topic, offering readers a one-stop solution for those working on fault-tolerant attitude control for spacecraft.


  • Presents the fundamentals of fault-tolerant attitude control systems for spacecraft in one practical solution
  • Gives the latest research and thinking on nonlinear attitude control, fault tolerant control, and reliable attitude control
  • Brings together concepts in fault control theory, fault diagnosis, and attitude control for spacecraft
  • Covers advances in theory, technological aspects, and applications in spacecraft
  • Presents detailed numerical and simulation results to assist engineers
  • Offers a clear, systematic reference on fault-tolerant control and attitude control for spacecraft
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Specificații

ISBN-13: 9780323898638
ISBN-10: 0323898637
Pagini: 304
Ilustrații: 125 illustrations (100 in full color)
Dimensiuni: 152 x 229 mm
Greutate: 0.41 kg
Editura: ELSEVIER SCIENCE

Cuprins

1. Overview 2. Preliminaries 3. Robust fault-tolerant attitude control 4. Fault-tolerant attitude control with actuator saturation 5. Fault-tolerant velocity-free attitude control 6. Fault-tolerant finite-time attitude-tracking control 7. Active fault-tolerant attitude control 8. Conclusions and future work