Design theory of thrust vector control servo mechanism for a type of spacecraft

[1] 王占林.近代电气液压控制[M].北京:北京航空航天大学出版社,2005:3-5 Wang Zhanlin.Modern electric hydraulic control[M].Beijing:Beijing University of Aeronautics and Astronautics Press,2005:3-5(in Chinese) [2] Charrier J,Kulshrshtha A.Electric actuation for flight & engine control system:evolution,current trends & future challenges .AIAA-2007-1391,2007 [3] Rodriguez F D.Electromechanical motion control system in spacecraft applications .AIAA-2006-7291,2006 [4] Albright J D,Moore L A.Development and implementation of electromechanical actuators for the X-38 atmospheric test vehicles .AIAA-2008-6569,2008 [5] 周元钧,赵运坤,葛云海.复合式余度机电作动系统容错控制与性能分析[J].北京航空航天大学学报,2008,34(3):285-289 Zhou Yuanjun,Zhao Yunkun,Ge Yunhai.Fault-tolerant control method and characteristic analysis of hybrid redundant EMA system[J].Journal of Beijing University of Aeronautics and Astronautics,2008,34(3):285-289(in Chinese) [6] Pan Zhiyang,Lou Fanglin.Novel soft switching inverter for brushless DC motor variable speed drive system[J].IEEE Transactions on Power Electronics,2004,19(2):280-288 [7] Garrison M,Steffan S.Two-fault tolerant electric actuation systems for space applications .AIAA-2006-4939,2006