supported by the National Natural Science Foundation of China (Nos. 61622304,61773201);the Natural Science Foundation of Jiangsu Province(No.BK20160035);the Fundamental Research Funds for the Central Universities (Nos. NE2014202,NE2015002)
We review the controllability research on spacecraft attitude based on nonlinear geometry control theory.The existing studies on attitude controllability are mostly concerning the global controllability and small time...