Spacecraft Attitude Control

A Linear Matrix Inequality Approach
Erscheinungsjahr 2022
ISBN: 978-0-323-99005-9
Verlag: William Andrew Publishing

Buch, Englisch, 384 Seiten, Format (B × H): 152 mm x 229 mm, Gewicht: 610 g

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.

Zielgruppe

Practicing professionals, undergraduate and graduate students in the field of spacecraft attitude control or control engineering and readers interested in the field of spacecraft attitude control or robust control systems

Autoren/Hrsg.

Liu, Chuang

Yue, Xiaokui

Shi, Keke

Sun, Zhaowei

Fachgebiete

• Technische Wissenschaften Elektronik | Nachrichtentechnik Nachrichten- und Kommunikationstechnik Regelungstechnik
• Technische Wissenschaften Verkehrstechnik | Transportgewerbe Luft- und Raumfahrttechnik, Luftverkehr

Inhaltsverzeichnis

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

Über Autor(innen)

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

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

Yue, Xiaokui
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.

Liu, Chuang
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.