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	Self-sacrificing templated formation of Co3O4/ZnCo2O4 composite hollow nanostructures for highly sensitive detecting acetone vapor 期刊论文 OAI收割 SENSORS AND ACTUATORS B-CHEMICAL, 2018, 卷号: 273, 页码: 1202-1210 作者: Thomas, Tiju; Qu, Fengdong; Zhang, Bingxue; Zhou, Xinxin; Zhang, Shendan \| 收藏 \| 浏览/下载：36/0 \| 提交时间：2018/12/04 Gas-sensing Properties Galvanic Replacement Selective Detection Designed Formation Ion Batteries Thin-films Sensors Performance Catalyst Sno2
	Self-sacrificing templated formation of Co3O4/ZnCo2O4 composite hollow nanostructures for highly sensitive detecting acetone vapor 期刊论文 OAI收割 SENSORS AND ACTUATORS B-CHEMICAL, 2018, 卷号: 273, 页码: 1202-1210 作者: Ruan, Shengping; Zhang, Shendan; Zhou, Xinxin; Zhang, Bingxue; Thomas, Tiju \| 收藏 \| 浏览/下载：37/0 \| 提交时间：2018/12/04 Gas-sensing Properties Galvanic Replacement Selective Detection Designed Formation Ion Batteries Thin-films Sensors Performance Catalyst Sno2
	Self-sacrificing templated formation of Co3O4/ZnCo2O4 composite hollow nanostructures for highly sensitive detecting acetone vapor 期刊论文 OAI收割 SENSORS AND ACTUATORS B-CHEMICAL, 2018, 卷号: 273, 页码: 1202-1210 作者: Qu, Fengdong; Thomas, Tiju; Zhang, Bingxue; Zhou, Xinxin; Zhang, Shendan \| 收藏 \| 浏览/下载：37/0 \| 提交时间：2019/12/18 GAS-SENSING PROPERTIES SELECTIVE DETECTION DESIGNED FORMATION THIN-FILMS PERFORMANCE CATALYST SENSORS SNO2 MICROSTRUCTURE ADSORPTION
	Adaptive control at launching using three loop autopilot (EI CONFERENCE) 会议论文 OAI收割 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China 作者: Zhang Y. 收藏 \| 浏览/下载：25/0 \| 提交时间：2013/03/25 In order to guarantee the precise initial flight trajectory control the missile disturbance of large disturbance torque three loop adaptive autopilot was researched. The characteristics of the projectile and three loop autopilot instruction formation characteristics were analysed. From equivalent pitching angle of lateral acceleration feedback loop combined with the instruction of generalized error autopilot structure was simplified and three loop autopilot adaptive control law and stability were designed. The test data show that when disturbance torque was 600Nm the attitude angle generalized error was -4.4. In the time lasted about 15s late trajectory accuracy was within 1.0.Three loop autopilot adaptive control law was able to control the disturbance of initial trajectory and adapt to dynamic characteristics changes control system stability. It was the initial trajectory accurate solution method of flight. 2011 IEEE.
	Motion mechanism analysis of a two-degree-of-freedom spherical motor (EI CONFERENCE) 会议论文 OAI收割 2nd International Conference on Information Engineering and Computer Science, ICIECS 2010, December 25, 2010 - December 26, 2010, Wuhan, China 作者: Guo K. 收藏 \| 浏览/下载：19/0 \| 提交时间：2013/03/25 The working principle of a two-degree-of-freedom piezoelectric spherical motor using only one piezoelectric element was analyzed. The resonance frequencies of the motor's plate type piezoelectric vibrator were calculated by finite element method. The computer simulation was executed to analyze the motion trajectory of the four contact points between the stator and the sphere. Simulation results verified that the four contact points can form timing reasonable elliptical trajectories which re designed to drive the sphere to form two rotation degrees of freedom. The conclusion indicated the formation of two-dimensional movement mechanism of the spherical motor. 2010 IEEE.
	Study and calibration of azimuth effect in multi-position strap-down north seeking system (EI CONFERENCE) 会议论文 OAI收割 7th World Congress on Intelligent Control and Automation, WCICA'08, June 25, 2008 - June 27, 2008, Chongqing, China 作者: Wang Z.; Zhao J.; Wang Z. 收藏 \| 浏览/下载：10/0 \| 提交时间：2013/03/25 In order to reduce the influence of azimuth effect in multi-position strap-down north seeking system its cause of formation is studied based on the precession principle of the dynamically tuned gyro. A detecting system composed by true north prism two Leica theodolites and benchmark prism fixed in the strap-down north seeking system was designed to calibrate the azimuth effect. By two steps many measurements are gone on in every position to eliminate the random error. According to the homologous between the error and the position a sinusoid is made a fit as compensate curve after the error of twelve positions is measured. Then the azimuth effect of the arbitrary position can be corrected by the curve. The experiment result shows that the seeking north standard deviation is only 11.77 after compensation which is considerably less than the 87.75 without correction. 2008 IEEE.