supported by the National Natural Science Foundation of China(Nos.62073165 and 62233009);the 111 Project,China(No.B20007).
This paper investigates fault tolerant attitude control theory and experiment for underactuated spacecraft with one reaction wheel completely broken and two others suffering actuator faults of partial loss of effectiv...
supported by Aeronautical Science Foundation of China (No. 2016ZC51025);the Open Research Fund of Key Laboratory of Space Utilization, Chinese Academy of Science (No. 20161201)
With the development of more/all electrical aircraft technology, an electro-mechanical actuator(EMA) is more and more used in an aircraft actuation system. The motor system, as the crucial part of an EMA, usually ad...
This paper proposes a novel fault tolerant control with torque limitation based on the fault mode for the ten-phase permanent magnet synchronous motor (PMSM) under various open-circuit and short-circuit fault condit...
supported by the Aeronautical Science Foundation of China(No.20101024006)
Abstract Multisensor systems are very powerful in the complex environments. The cointegration theory and the vector error correction model, the statistic methods which widely applied in economic analysis, are utilized...
support from the National Natural Science Foundation of China;the Fundamental Research Funds for the Central Universities of China
Abstract Single event upset (SEU) effect, caused by highly energized particles in aerospace, threatens the reliability and security of small satellites composed of commercialofftheshelves (COTS). SEU induced contr...
Improving fault tolerant performance of permanent magnet synchronous motor has always been the central issue of the electrically supplied actuator for aerospace application. In this paper, a novel fault tolerant perma...