Spacecraft Attitude Control: A Linear Matrix Inequality Approach

ISBN-13: 9780323990059 / Angielski / Miękka / 2022 / 386 str.

Zhaowei Sun; Keke Shi; Xiaokui Yue

Spis treści

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

O autorze

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.