Roll-pitch-yaw autopilot design for nonlinear time-varying missile using partial state observer based global fast terminal sliding mode control
terminal sliding mode control、environmental conditions、nonlinear observer、system stability、great challenge、flight envelope、coupling effect、control signals、sign function、state vector、closed loop、in order
29
TP3;TP2
This work is co-supported by the National Natural Science Foundation of China61304077;International Science& Technology Cooperation Program of China2015DFA01710;the Natural Science Foundation of Jiangsu Province of ChinaBK20130765;the Chinese Ministry of Education Project of Humanities and Social Sciences13YJCZH171;the 11th Jiangsu Province Six Talent Peaks of High Level Talents Project of China2014_ZBZZ_005;the Jiangsu Province Project Blue:Young Academic Leaders Project
2016-11-10(万方平台首次上网日期,不代表论文的发表时间)
共11页
1302-1312