Fast Satellite Attitude Maneuver and Control
Published on 3. August 2022
Book
Paperback/Softback
278 pages
978-0-323-95455-6 (ISBN)
Description
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.
It will be an excellent resource for researchers working on spacecraft design, nonlinear control systems, vehicle systems and complex control systems.
More details
Series
Language
English
Place of publication
Oxford
United Kingdom
Publishing group
Elsevier Science & Technology
Target group
Professional and scholarly
Aerospace engineers working on spacecraft design; Control engineers working on nonlinear control systems; Mechanical engineers working on vehicle systems; Mathematicians and physician working on complex and nonlinear control systems; Postgraduate students majoring on aerospace engineering, mechatronics, control engineering, mechanical engineering, and applied mathematics
Practitioners working on spacecraft control systems; Mathematicians and physician working on nonlinear dynamic systems; 3rd/4th-year students who are interested in knowing advances in spacecraft attitude control system
Dimensions
Height: 152 mm
Width: 229 mm
Thickness: 19 mm
Weight
450 gr
ISBN-13
978-0-323-95455-6 (9780323954556)
Copyright in bibliographic data and cover images is held by Nielsen Book Services Limited or by the publishers or by their respective licensors: all rights reserved.
Schweitzer Classification
Other editions
Additional editions
Dong Ye | You Li | Yan Xiao
Fast Satellite Attitude Maneuver and Control
E-Book
08/2022
Academic Press
€140.00
Available for download
Persons
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. You Li graduated from Harbin Institute of Technology in 2017, and now is a Lecturer at the School of Aerospace Science and Technology, Xidian University, in China. His work is mainly focusing on satellite attitude control, especially on satellite attitude fast maneuver. Yan Xiao received his Ph.D. degree in Aeronautical and Astronautical Science and Technology from the Harbin Institute of Technology (HIT) and now is an Assistant Professor at the School of Astronautics, HIT. His current research interests include nonlinear control, spacecraft attitude dynamics and control, coordination control, etc.
Content
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
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