Controllability of Spacecraft Attitude and Its Application in Reconfigurability Analysis

• 作 者: YANG Hao MENG Qingkai JIANG Bi
• 机 构: CollegeofAutomationEngineering
• 出 处: 南京航空航天大学学报:英文版
• 发表日期: 2019年2期
• 关键词: CONTROLLABILITY SPACECRAFT ATTITUDE CONTROL geometry CONTROL theory fault.tolera
• 基金项目: 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(No

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 local controllability(STLC).A present