“…Therefore, the aforementioned demanding problems of spacecraft attitude control 3 provoked a range of profound considerations. In recent decades, to achieve rapid maneuvering, flexible tracking, high-precision pointing, and other desired performances, numerous control strategies are proposed to accurately provide corresponding attitude changes, such as the adaptive control, 4,5 backstepping control, 6,7 fault-tolerant control (FTC), [8][9][10] and disturbance observer (DO)-based control. 11 For the purpose of eliminating the influence of the unknown nonlinearities and uncertainties, [12][13][14][15] extensive researches have been carried out by scholars.…”