supported by the National Basic Research Program of China(973 Program)(No.2014CB046402);the National Natural Science Foundation of China(Nos.51575019,51305011);the 111 Program of China
This paper presents an integrated fuzzy controller design approach to synchronize a dis- similar redundant actuation system of a hydraulic actuator (HA) and an electro-hydrostatic actu- ator (EHA) with system unce...
supported by the Aeronautical Science Foun-dation of China(No.2012XX51043);‘‘Fanzhou’’Youth Scientific Funds of China(No.20100504)
A large-scale high altitude environment simulation test cabin was developed to accurately control temperatures and pressures encountered at high altitudes. The system was developed to provide slope-tracking dynamic co...
supported by the Fundamental Research Funds for the Central Universities of China
In this paper, a novel vibration-suppression open-loop control method for multi-mass system is proposed, which uses two-stage velocity compensating algorithm and fuzzy I + P control- ler. This compensating method is ...
supported by the Aeronautical Science Foundation of China(No.2012ZD51043);‘‘Fanzhou’’ Youth Scientifc Funds(No.20100504)
The structure and characteristics of a large multi-parameter environmental simulation cabin are introduced.Due to the diffculties of control methods and the easily damaged characteristics,control systems for the large...
co-supported by National Natural Science Foundation of China (Nos. 91116017, 60974106 and 11102080);Funding for Outstanding Doctoral Dissertation in NUAA (No. BCXJ10-04)
An adaptive robust attitude tracking control law based on switched nonlinear systems is presented for a variable structure near space vehicle (VSNSV) in the presence of uncertainties and disturbances. The adaptive f...
National High-tech Research and Development Program of China (2009AA04Z412);"111" Project;BUAA Fund of Graduate Education and Development
Passive torque servo system (PTSS) simulates aerodynamic load and exerts the load on actuation system, but PTSS endures position coupling disturbance from active motion of actuation system, and this inherent disturb...
A single gimbal control moment gyro system is the best choice for large spacecraft attitude control systems, as executive components of spacecraft guidance, navigation, and control system. But the phenomenon of singul...
Pre-research subject of the 9-th 5 year plan for National Defenc
The transistor voltage regulators have been widely adopted in the brushless AC generators in aircraft. This paper researches the digital voltage regulator. The paper presents the hardware platform of the digital volta...