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	The effects of interfaces stability on mechanical properties, thermal conductivity and helium irradiation of V/Cu nano-multilayer composite 期刊论文 OAI收割 MATERIALS & DESIGN, 2022, 卷号: 216 作者: Zhang, L. F.; Gao, R.; Hou, J.; Zeng, L. F.; Xin, J. J. \| 收藏 \| 浏览/下载：28/0 \| 提交时间：2022/12/23 Cross accumulative roll bonding Nano-multilayer composite Microstructure stability Thermal conductivity Helium irradiation
	Reaction-Wheel-Based Roll Stabilization for a Robotic Fish Using Neural Network Sliding Mode Control 期刊论文 OAI收割 IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2020, 卷号: 25, 期号: 4, 页码: 1904-1911 作者: Zhang, Pengfei; Wu, Zhengxing; Dong, Huijie; Tan, Min; Yu, Junzhi \| 收藏 \| 浏览/下载：42/0 \| 提交时间：2020/09/28 Mobile robots Wheels Rotors Robot sensing systems Stability analysis Mechatronics Neural network feedforward control reaction wheel robotic fish roll stability sliding mode control
	The application of charge transfer host based exciplex and thermally activated delayed fluorescence materials in organic light-emitting diodes 期刊论文 OAI收割 Organic Electronics, 2019, 卷号: 66, 页码: 227-241 作者: Z.Q.Wang; C.Wang; H.Zhang; Z.M.Liu; B.Zhao \| 收藏 \| 浏览/下载：34/0 \| 提交时间：2020/08/24 OLED,Exciplex,TADF,Host,low roll-off,external quantum efficiency,high-power efficiency,highly,efficient,high-performance,energy-transfer,color stability,triplet,energy,blue exciplex,hybrid woleds,Materials Science,Physics
	Research on model reference sliding mode control in roll stabilization of aerocraft (EI CONFERENCE) 会议论文 OAI收割 2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China Chu H.-R. 收藏 \| 浏览/下载：39/0 \| 提交时间：2013/03/25 Aimed at aerospace roll stabilization control arithmetic based on model reference sliding mode variable structure theory and chattering reduction arithmetic are formulated. Correctness and validity of arithmetic are analyzed. With flight dynamics the roll-loop mathematic model and reference model are established. Sliding hyperplane is deduced based on model reference sliding mode variable structure theory. Combing with reaching law control law is derived and stability of roll-loop is analyzed. Chattering of aileron instructions is alleviate by using boundary layer approach. Digital flying simulation result shows that variable structure control arithmetic realized roll stabilization control the roll angle is less than 5.3 under powered flight and that of unpowered flight is less than 0.5 respectively. The command fin angle is less than 1.5. High frequency chattering of fin command nearby the minimum velocity was trailed off by chattering reduction arithmetic. The sliding mode control arithmetic show good performance when aerodynamic coefficients varies 20%. The control arithmetic is easy to be implemented for its simplicity. 2011 IEEE.
	Control method research on wide flight envelope aerocraft (EI CONFERENCE) 会议论文 OAI收割 2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China 作者: Duan Z. 收藏 \| 浏览/下载：27/0 \| 提交时间：2013/03/25 The flying qualities of aerocraft was directly effected by the autopilot for the wide flight envelope aerocraft on the basic of analyzing the typical trajectory the three loop autopilots of roll stability pitch and yaw were designed using single-mode Transient suppression method the overload due to control surface transition deflection was avoided when control parameters changing the verification was done by non-linear simulation. The result showed that: Under the action of the disturbance torque the maximum roll was less than 5 the range of the aerocraft was from 13.5km to 22.4km the max height was about 5100m the max deviation of lateral was about 42m the maximum elevator deflection was less than 6.5 the control law was applicable within the effective range. An autopilot design method of wide flight envelope aerocraft was provided. 2011 IEEE.