Dong Ye, You Li, Yan Xiao

Fast Satellite Attitude Maneuver and Control

• Broschiertes Buch

Produktbeschreibung

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.

Produktdetails

• Emerging Methodologies and Applications in Modelling, Identification and Control
• Verlag: Academic Press / Elsevier Science & Technology
• Artikelnr. des Verlages: C2021-0-03404-0
• Seitenzahl: 278
• Erscheinungstermin: 3. August 2022
• Englisch
• Abmessung: 152mm x 229mm x 19mm
• Gewicht: 450g
• ISBN-13: 9780323954556
• ISBN-10: 0323954553
• Artikelnr.: 63512327

Autorenporträt

Dong Ye is a Professor at the School of Astronautics, Harbin Institute, in China. His research interests include spacecraft dynamics and control and hardware-in-the-loop simulation technique.

Inhaltsangabe

1. Introduction and Literature Review
2. Preliminaries and Mathematical Model
3. Near Time-Optimal Control Based on Analytical Trajectory Planning
4. Time Efficient Robust PID Plus Control with Constraints
5. Bang-Bang Logic-based Time Efficient Sliding Mode Control
6. Robust Finite Time Control Based on Three Stage Structure Sliding Mode
7. Finite Time Output Feedback Attitude Control
8. Observer-Based Continuous Finite-Time Attitude Control
9. Neural Network-Based Finite Time Fault-Tolerant Attitude Control
10. Hybrid Thrusters and Reaction Wheels based Attitude Control with High Precision
11. Finite Time Attitude Control with Hybrid Actuators
12. A Control Allocation Approach for Hybrid Actuator
13. Conclusions and Future Works