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空间光通信终端精跟踪伺服系统研究 被引量:7
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作者 黎明 艾勇 曹阳 《激光技术》 CAS CSCD 北大核心 2009年第3期262-265,共4页
为了提高空间光通信中的精跟踪伺服系统的跟踪精度,采用神经网络比例-积分-微分算法,解决精跟踪伺服系统设计中光斑抖动时变不确定性和压电陶瓷驱动中存在的迟滞、蠕变和位移非线性等不足。通过3层结构反向传播神经网络自学习方法,在线... 为了提高空间光通信中的精跟踪伺服系统的跟踪精度,采用神经网络比例-积分-微分算法,解决精跟踪伺服系统设计中光斑抖动时变不确定性和压电陶瓷驱动中存在的迟滞、蠕变和位移非线性等不足。通过3层结构反向传播神经网络自学习方法,在线调整比例-积分-微分控制器的系数,控制压电陶瓷驱动精瞄偏转镜偏转,最终达到精跟踪伺服系统优化控制。进行了理论分析和实验验证,取得了室内精跟踪数据。结果表明,神经网络比例-积分-微分控制算法增强了伺服系统鲁棒性,并提高了伺服系统实时性;采用400Hz 的 CCD,精跟踪伺服系统对40Hz 以下的抖动能有效抑制,基本能满足在空间光通信中跟踪带宽需要。 展开更多
关键词 光通信 精跟踪 自适应神经网络比例-积分-微分控制器 压电陶瓷驱
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Micro-displacement amplifying mechanism driven by piezoelectric actuator 被引量:10
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作者 马浩全 胡德金 张凯 《Journal of Southeast University(English Edition)》 EI CAS 2004年第1期75-79,共5页
Piezoelectric actuator has high stiffness, high frequency and infinite control precision, but a short output displacement which is often 1/1 000 of its length. In order to meet the requirements that tools feeding shou... Piezoelectric actuator has high stiffness, high frequency and infinite control precision, but a short output displacement which is often 1/1 000 of its length. In order to meet the requirements that tools feeding should be long-travel, high-frequency and high-precision in non-circular precision turning, a new one-freedom flexure hinge structure is put forward to amplify the output displacement of piezoelectric actuator. Theoretical analysis is done on the static and dynamic characteristics of the structure, differential equations are presented, and it is also verified by the finite element method. It's proved by experiments that the output displacement of the structure is 293 μm and its resonant frequency is 312 Hz. 展开更多
关键词 piezoelectric actuator flexure hinge micro displacement amplifying structure
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液压放大式PZT-DDV建模与控制仿真 被引量:2
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作者 俞军涛 焦宗夏 吴帅 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2013年第10期1354-1359,共6页
研制基于液压位移放大原理的压电陶瓷直接驱动伺服阀(PZT-DDV,Piezoelectric-Direct Drive Valve),实现大流量高频响的要求.分析其结构特点,建立系统数学模型,基于AMESim和Simulink的协同仿真环境,对其进行仿真控制研究.采用AMESim建立... 研制基于液压位移放大原理的压电陶瓷直接驱动伺服阀(PZT-DDV,Piezoelectric-Direct Drive Valve),实现大流量高频响的要求.分析其结构特点,建立系统数学模型,基于AMESim和Simulink的协同仿真环境,对其进行仿真控制研究.采用AMESim建立了PZTDDV的模型和虚拟液压测试系统,利用Simulink建立了数字控制器模型,通过接口组成协同仿真环境.针对PZT-DDV的迟滞、摩擦和液压位移放大结构的负载敏感特性,采用前馈控制改善迟滞,提高动态响应.基于LuGre摩擦力模型以及密闭腔压力监测,采用自适应backstepping方法实现摩擦及负载变化对放大机构输出位移的扰动补偿.仿真结果表明:前馈控制提高了系统的动态性能,自适应backstepping控制方法提高了系统的稳态控制精度. 展开更多
关键词 压电陶瓷 液压放大 迟滞、摩擦、负载敏感 前馈控制 BACKSTEPPING控制
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THEORETICAL AND EXPERIMENTAL STUDY ON THE PIEZOCERAMIC ACTUATING LAMINATE
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作者 万建国 陶宝祺 朱纪军 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 1997年第1期90-97,共8页
Piezoelectric ceramic element (PCE) is a kind of actuator applied widely on the intelligent material & structure. Establishing the relationship between the transferring stress and the controlling signal, namely t... Piezoelectric ceramic element (PCE) is a kind of actuator applied widely on the intelligent material & structure. Establishing the relationship between the transferring stress and the controlling signal, namely the transferring and actuating equation, is a key step to analyze the actuating performance of the PCE. Based on the method of the shear lag theory, the procedure of the stress transferring is analyzed and the transferring and actuating model is established in this paper. Some measurements for PCE(PZT5) actuating the Glass Fiber/Epoxy laminate have been done to verify the model established. The experimental results show that the theoretical model agrees well with the practice. Finally, the effect of the main factors on PCE actuating the laminate is studied by using the experimental and theoretical results. 展开更多
关键词 piezoelectric ceramics LAMINATES actuate transfer affecting factors
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An automated AFM for nanoindentation and force related measurements
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作者 BAI Jiang-hua Andres La Rosa 《Journal of Measurement Science and Instrumentation》 CAS CSCD 2018年第4期347-353,共7页
A fully automated atomic force microscope(AFM)is presented.The mechanical motion of the AFM stage was controlled by three steppers.The fine motion of the AFM was controlled by an MCL one-axis piezo plate.A32.768kHz cr... A fully automated atomic force microscope(AFM)is presented.The mechanical motion of the AFM stage was controlled by three steppers.The fine motion of the AFM was controlled by an MCL one-axis piezo plate.A32.768kHz crystal tuning fork(TF)was used as the transducer with a probe attached.An acoustic sensor was used to measure the interactions between the probe and the sample.An SR850lock-in amplifier was used to monitor the TF signals.An additional lock-in amplifier was used to monitor the acoustic signal.A field programmable gate array(FPGA)board was used to collect the data in automatic mode.The main controller was coded with LabVIEW,which was in charge of Z-axis scan,signal processing and data visualization.A manual mode and an automatic mode were implemented in the controller.Users can switch the two modes at any time during the operation.This AFM system showed several advantages during the test operations.It is simple,flexible and easy to use. 展开更多
关键词 atomic force microscope(AFM) nano indentation acoustic sensing piezo drive crystal tuning fork LabVIEW lock-in amplifier 8051microcontroller
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Active control of fluctuating pressure induced by blade-vortex interaction 被引量:4
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作者 ZHANG MingMing XU JianZhong 《Science China(Technological Sciences)》 SCIE EI CAS 2011年第4期862-868,共7页
It is well known that interactions between the leading edge of a blade and incoming vortical structures produce a sharp rise in fluctuating pressure nearby,contributing significantly to the noise production in various... It is well known that interactions between the leading edge of a blade and incoming vortical structures produce a sharp rise in fluctuating pressure nearby,contributing significantly to the noise production in various types of rotorcrafts.To suppress this fluctuating pressure and subsequently induced noise,as the first step,active control of interactions between an airfoil and incoming cylinder-generated vortices,which mimics the practical phenomenon,was experimentally investigated.The essence of the control is to create a local perturbation,using piezo-ceramic actuators,on the surface near the leading edge of the airfoil,thus modifying the airfoil-vortex interactions.Both open-and closed-loop methods were used,where the surface perturbation was controlled by an external sinusoidal wave and a feedback pressure signal from a pressure transducer installed at the leading edge,respectively.It was observed that the closed-loop control was superior to the open-loop one;the closed-and open-loop controls achieve a maximum reduction in the pressure fluctuation at the dominant vortex frequency by 32% and 11%,respectively.The detailed physics behind the observations was discussed. 展开更多
关键词 blade-vortex interaction perturbation technique piezo-ceramic actuator closed-loop control
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