Spacecraft Attitude Control: A Linear Matrix Inequality Approach

by Chuang Liu, Xiaokui Yue, Keke Shi, Zhaowei Sun

Overview

Spacecraft Attitude Control: A Linear Matrix Inequality Approach solves problems for spacecraft attitude control systems using convex optimization and, specifi cally,
through a linear matrix inequality (LMI) approach. High-precision pointing and improved robustness in the face of external disturbances and other uncertainties are requirements for the current generation of spacecraft. This book presents an LMI approach to spacecraft attitude control and shows that all uncertainties in the maneuvering process can be solved numerically. It explains how a model-like state space can be developed through a mathematical presentation of attitude control systems, allowing the controller in question to be applied universally. The authors describe a wide variety of novel and robust controllers,
applicable both to spacecraft attitude control and easily extendable to second-order systems. Spacecraft Attitude Control provides its readers with an accessible introduction to spacecraft attitude control and robust systems, giving an extensive survey of current research and helping researchers improve robust control performance.

Product Details

ISBN-13:	9780323990059
Publisher:	Elsevier Science
Publication date:	02/04/2022
Pages:	384
Product dimensions:	6.00(w) x 9.00(h) x 0.80(d)

About the Author

Chuang Liu is an Associate Professor at Northwestern Polytechnical University, China. He is also Scientific Committee Member of Aeromeet 2022. He received the COSPAR Outstanding Paper Award for Young Scientists in 2020. His research focuses on aerospace engineering.

Xiaokui Yue is a Professor at Northwestern Technical University, China. His research has focused on the frontiers of space exploration and on computational methods for nonlinear dynamical systems.

Keke Shi is a Research Assistant at the Harbin Institute of Technology, China. His research is focused on overall spacecraft design and dynamics control.

Zhaowei Sun is a Professor at the Harbin Institute of Technology, China. His research focuses on overall spacecraft dynamics and control.

Table of Contents

1. Introduction of basic knowledge
2. State feedback nonfragile control
3. Dynamic output feedback nonfragile control
4. Observer-based fault tolerant delayed control
5. Observer-based fault tolerant nonfragile control
6. Disturbance observer-based control with input magnitude and rate constraints
7. Improved mixed H2/HN control with poles assignment constraint
8. Nonfragile HN control with input constraints
9. Antidisturbance control with active vibration suppression
10. Chaotic attitude tracking control
11. Underactuated chaotic attitude stabilization control

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From the Publisher

Presents solutions to spacecraft attitude control systems using a linear matrix inequality (LMI) approach