Spacecraft Attitude Control
Liu, Chuang (Associate Professor, Northwestern Polytechnical University, China) / Yue, Xiaokui (Professor, Northwestern Technical University, China) / Shi, Keke (Research Assistant, Harbin Institute of Technology, China) / Sun, Zhaowei (Professor, Harbin Institute of Technology, China)
The attitude maneuvering process for spacecraft involves uncertainties for both rigid and flexible spacecraft, leading to chaotic motion. Analytic solutions to these problems do exist, but in all cases they can be solved through numerical methods. Specifically, uncertainties in controllers can be reduced through a linear matrix inequalities (LMI) approach. Spacecraft Attitude Control:A Linear Matrix Inequality Approach presents solutions to sp...
