机译:基于PD型状态反馈和线性矩阵不等式的特殊正交群SO(3)的鲁棒姿态跟踪
Department of Aeronautics & Astronautics, Institute of Space Technology, Islamabad, Pakistan;
Attitude control; Special Orthogonal Group SO(3); Nonlinear H_∞ control; Linear matrix inequalities; Controller synthesis;