首页|期刊导航|南京航空航天大学学报（英文版）|Robust Fault-Tolerant Control for Longitudinal Dynamics of Aircraft with Input Saturation
南京航空航天大学学报（英文版）2016，Vol.33Issue(3)：319-328,10.
Robust Fault-Tolerant Control for Longitudinal Dynamics of Aircraft with Input Saturation
Robust Fault-Tolerant Control for Longitudinal Dynamics of Aircraft with Input Saturation
摘要
关键词
longitudinal dynamics/input saturation/detection observer/fault-tolerant control/aircraftsKey words
longitudinal dynamics/input saturation/detection observer/fault-tolerant control/aircrafts分类
信息技术与安全科学引用本文复制引用
Yang Qingyun,Chen Mou..Robust Fault-Tolerant Control for Longitudinal Dynamics of Aircraft with Input Saturation[J].南京航空航天大学学报（英文版）,2016,33(3):319-328,10.基金项目
This work was supported by the National Natural Science Foundations of China (No.61573184,61374212),the Natural Science Foundation of Jiangsu Province,China (No.SBK20130033),the Specialized Research Fund for the Doctoral Program of Higher Education (No.20133218110013),and the Six Talents Peak Project of Jiangsu Province of China (No.2012CXXRJ-010). （No.61573184,61374212）
