Suppression of servo error uncertainty to 10^(-18)level using double integrator algorithm in ion optical clock

A universal locking model for single ion optical clocks was built based on a simple integrator and a double integrator.Different integrator algorithm parameters have been analyzed in both numerical simulations and experiments.The frequency variation measured by the comparison of two optical clocks coincides well with the simulation results for different second integrator parameters.According to the experimental results,the sensitivity of the servo error influenced by laser frequency drift with the addition of a double integrator was suppressed by a factor of 107.In a week-long comparison of optical clocks,the relative uncertainty of the servo error is determined to be 1.9×10^(-18),which is meaningful for the systematic uncertainty of the transportable single^(40)Ca^(+)ion optical clock entering the 10^(-18)level.

TWO-COORDINATE DUAL-SERVO CONTOURERROR COMPENSATION TECHNOLOGY FOR ULTRA-PRECISION MANUFACTURING

A technology of two-coordinate dual-servo(TCDS) is proposed. Using this technology which is based on error compensation, workpieces of higher contour accuracy could he turned on ultra-precision machine tool with Poor dynamic performances. The principle, constitute and operation of a TCDS system are described. Mathematical proof and experiments are achieved in addition.

ZERO PHASE ERROR REAL TIME CONTROL FOR FLIGHT SIMULATOR SERVO SYSTEM

Flight simulator is an important device and a typical high performanceposition servo system used in the hardware-in-the-loop simulation of flight control system. Withoutusing the future desired output, zero phase error controller makes the overall system's frequencyresponse exhibit zero phase shift for all frequencies and a very small gain error at low frequencyrange can be achieved. A new algorithm to design the feed forward controller is presented, in orderto reduce the phase error, the design of proposed feed forward controller uses a modified plantmodel, which is a closed loop transfer function, through which the system tracking precisionperformance can be improved greatly. Real-time control results show the effectiveness of theproposed approach in flight simulator servo system.

Zero phase error control based on neural compensation for flight simulator servo system

Using the future desired input value, zero phase error controller enables the overall system＇s frequency response exhibit zero phase shift for all frequencies and a small gain error at low frequency range, and based on this, a new algorithm is presented to design the feedforward controller. However, zero phase error controller is only suitable for certain linear system. To reduce the tracking error and improve robustness, the design of the proposed feedforward controller uses a neural compensation based on diagonal recurrent neural network. Simulation and real-time control results for flight simulator servo system show the effectiveness of the proposed approach.

激光跟踪测量系统伺服跟踪控制方法

针对激光跟踪测量系统跟踪目标的运动轨迹不确定、加速度与速度不断变化的特点,为提升其稳态及动态性能,对伺服跟踪控制方法进行研究,提出一种基于模糊自适应的激光跟踪双闭环控制方法。电机定位控制环路采用模糊自适应微分先行PID,位置跟踪控制环路采用模糊自适应整定PI,设计不同模糊规则,实现控制参数实时整定,使其始终保持在最优区间。实验结果表明,该方法能够根据跟踪目标运动的不确定性产生的误差来实时调整控制参数,有效提升激光跟踪的稳态和动态性能,使跟踪系统的稳态误差降低至1.90′以内,跟随误差则降低至0.56′以内。

Modified wavelet filtering algorithm applied to gyro servo technology for the improvement of test-precision

In order to improve the measurement-precision of the gyro,the gyro experiment is completed based on gyro servo technology.The error sources of gyro servo technology are analyzed in the process of measurement,and the impact of these error sources on measurement is evaluated.To eliminate interference signal existing in the sampled data of the measurement,a modified wavelet threshold filtering method is presented.The results of the simulation and measurement show that the estimation-precision of the proposed method is improvement remarkably compared with the fast Fourier transform method,and the calculation work is reduced compared with the conventional wavelet threshold filtering methods,furthermore,the phenomenon of a common threshold of ＂killing＂ is solved thoroughly.

Controller Parameter Tuning of Delta Robot Based on Servo Identification

High-speed pick-and-place parallel robot is a system where the inertia imposed on the motor shafts is real-time changing with the system configurations.High quality of computer control with proper controller parameters is conducive to overcoming this problem and has a significant effect on reducing the robot＇s tracking error.By taking Delta robot as an example,a method for parameter tuning of the fixed gain motion controller is presented.Having identifying the parameters of the servo system in the frequency domain by the sinusoidal excitation,the PD＋feedforward control strategy is proposed to adapt to the varying inertia loads,allowing the controller parameters to be tuned by minimizing the mean square tracking error along a typical trajectory.A set of optimum parameters is obtained through computer simulations and the effectiveness of the proposed approach is validated by experiments on a real prototype machine.Let the traveling plate undergoes a specific trajectory and the results show that the tracking error can be reduced by at least 50%in comparison with the conventional auto-tuning and Z-N methods.The proposed approach is a whole workspace optimization and can be applied to the parameter tuning of fixed gain motion controllers.

QFT control based on zero phase error compensation for flight simulator

To improve the robustness of high-precision servo systems, quantitative feedback theory （QFT） which aims to achieve a desired robust design over a specified region of plant uncertainty is proposed. The robust design problem can be solved using QFT but it fails to guarantee a high precision tracking. This problem is solved by a robust digital QFT control scheme based on zero phase error （ZPE） feed forward compensation. This scheme consists of two parts： a QFT controller in the closed-loop system and a ZPE feed-forward compensator. Digital QFT controller is designed to overcome the uncertainties in the system. Digital ZPE feed forward controller is used to improve the tracking precision. Simulation and real-time examples for flight simulator servo system indicate that this control scheme can guarantee both high robust performance and high position tracking precision.

ON GENERAL TYPE OF DIGITAL OPTIMAL PREVIEW SERVO SYSTEM

Usually, only siep future desired singals are utilized in the field of preview servo systems design. In this paper, we discuss the design problem of optimal preview servo system while the future desired signal and future disturbance signal are polynomials or outputs of linear free systems. (1) Conditions of controllability and observability for enlarged system, (2) a design method of optimal preview servo controllers, and (3) a simple and convenient algorithm of control law are obtained.

RESEARCH ON PREVIEW CONTROL TECHNIQUE BASED ON EXTENDED ERROR SYSTEM WITH DELAY

A valid preview control technique is presented for processing servo systemswith input delay based on extended error systems with input delay. The technique usesthe concept of error systems, establishes extended error systems with input delay and de-rives preview control laws based on minimization of evaluation function. Finally, simula-tion is done on linear direct current motor without brush. The results reveal that the tech-nique proposed herein is valid for improving performance of servo systems.

不同控制方式下伺服万能试验机控制误差实测分析

利用合金试件,应用250 kN电子万能试验机,设计同步加载试验,进行不同加载方式下伺服万能试验机控制误差实测研究及理论分析。试验结果显示:力控制方式的控制误差大于位移控制方式;力控制方式下,控制误差随加载速率的增大而增大,其调节时间与加载速率呈指数及对数关系;位移控制方式下,控制误差随加载速率变化不明显,其调节时间与加载速率呈幂函数关系;力控制方式循环编程控制误差更大,位移控制方式循环编程控制误差更小。理论分析表明:万能试验机采用梁型应变式载荷传感器及加载极性不同是造成力控制方式控制误差大于位移控制的主要原因。

基于动态理论模型的电液伺服加载前馈补偿复合控制系统

针对一般电液伺服系统存在的非预期负载扰动和非线性干扰等问题,为了提高系统的自适应能力和动态响应的品质,减小系统跟踪和输出响应的误差,提出了一种基于动态理论模型的电液伺服加载前馈补偿复合控制方法。首先,阐释了电液伺服试验台的结构组成及其数学模型,分析了系统力矩控制和位置控制的结构关系;然后,论证了自适应前馈补偿复合控制的伺服原理,阐述了以调速理论模型和实际模型的误差函数作为调速依据的前馈补偿和复合控制的原理和方法;最后,进行了系统仿真,同时为了验证基于动态理论模型的自适应前馈补偿复合控制策略的合理性和有效性,对伺服系统进行了加载试验。研究结果表明:采用该复合控制策略可以精确算出对伺服马达进行转速补偿的基准值和调整参数,系统动态响应速度比采用传统闭环控制算法提高了8%以上;系统控制器自适应能力和抗扰动性能也明显优于采用传统PI闭环控制及模糊PI闭环控制算法的系统;通过对比分析0.2 Hz和0.5 Hz的正弦响应曲线可知,该系统的位置跟踪曲线性能最优,控制精度最高,实际输出值的误差也最小。

面向EtherCAT总线的伺服系统误差及插补算法误差辨识方法

目前,工业运动控制中多采用EtherCAT总线进行主站和从站之间的通信,在EtherCAT总线上传输着大量的运动数据信息。基于此,提出一种面向EtherCAT总线的伺服系统误差及插补算法误差辨识方法。此方法通过ET2000和Wire-Shark抓获运动过程中EtherCAT总线上的数据,筛选有效数据生成pcapng文件,再对此文件和运动控制系统的ENI xml文件进行解析获得目标位置和实际位置信息,最后对得到的位置信息进行误差分析。针对各类误差设计了相应的运动轨迹,在机床上对单轴点位运动、两轴插补运动及两轴前瞻插补运动进行了多组运动控制实验,完成了伺服响应滞后、伺服动态性能不匹配、跟随误差、位置到位抖动以及插补算法误差等的辨识,通过此方法可获得单轴的运动控制精度以及多轴运动之间相互配合的能力。

飞机襟翼阀控伺服作动系统动态性能分析

由于阀控伺服作动系统存在的非线性因素,传统的建模方法所建立的数学模型无法准确地反映系统实际情况。为提升液压系统的控制精度及动态响应性能,解决在实际系统试验中出现的动态特性超差问题,对可能引起的因素及关键参数进行研究,重点分析引起系统静态误差的主要因素,同时分析系统各关键元件的固有频率和阻尼比对系统动态性能的影响。利用Matlab/Simulink软件对系统进行非线性建模,理论推导计算及仿真结果分析表明,较高的系统各关键元件固有频率和阻尼比有利于提高系统动态性能。

基于热误差补偿的行星滚柱丝杠综合性能试验台设计与分析

行星滚柱丝杠综合性能是丝杠性能的主要指标,现有测试系统多以静态测量法进行测量,操作复杂且偶然误差较高。通过对行星滚柱丝杠综合性能动态测试系统的试验原理、硬件设计、软硬件通讯、软件界面结构的研究,设计了一套行星滚柱丝杠综合性能动态测试系统。基于LabVIEW设计上位机人机交互与控制监测软件对丝杠热伸长量进行了检测,并使用最小二乘法分析丝杠温升与位移的关系,对定位精度试验进行误差补偿。实验结果表明,所设计的试验台系统可以测量行星滚柱丝杠定位精度、噪声、温升、极限转速、加速度,同时热误差测量补偿系统可以减小温度变化对测量位置的影响,补偿前后精度测量指标提升均在30%以上,偶然性误差较小并且精度提高。

数控机床伺服控制系统误差补偿及加工质量优化

随着科学技术的快速发展进步,数控机床的功能日渐完善,在机械制造业应用普及程度不断提升,已成为现代加工领域的重要基础设备。在实际加工过程中,应用伺服控制系统的数控机床尽管技术先进,但仍不可避免因存在系统误差而导致加工质量降低。该文结合伺服控制系统特征分析了数控机床的伺服控制系统在制造过程中的误差来源,介绍了误差补偿的有效方法,并给出了伺服控制下数控机床加工质量的优化方式,以期为提高数控机床加工精度提供理论支持。

伺服轴系装配精度提升研究

针对伺服转台轴系装配误差问题,开展伺服轴系误差研究,提出基于装配过程的误差检测和提取方法,通过优化各工艺参数,减小轴系装配各分误差,提升轴系装配精度,以期为同类产品装配提供借鉴。

基于非线性状态空间控制的伺服液压执行器跟踪误差仿真研究

目前,伺服液压执行器控制系统不仅响应速度慢,而且执行器运动位移跟踪精度也相对较低。对此,本文设计了非线性状态空间控制方法,并对伺服液压执行器响应速度和跟踪误差进行仿真。建立了伺服液压执行器平面简图,推导出液压执行器运动方程式。针对传统线性控制方法进行改进,利用系统的非线性状态空间模型,通过非线性反馈和坐标变换转化为线性可控系统,给出了非线性状态空间控制流程。针对不同环境条件下的信号波形,采用Matlab软件对伺服液压执行器响应速度和跟踪误差进行仿真,并且与线性控制效果进行比较。仿真结果表明:采用线性控制的伺服液压执行器,执行器响应速度慢、运动位移跟踪误差大,容易受到外界波形的干扰。采用非线性状态空间控制的伺服液压执行器,执行器响应速度快、运动位移跟踪误差较小,能够抑制外界波形的干扰。该执行器能够有效地抑制外界波形的干扰,不仅可以提高伺服液压执行器的响应速度,而且还能降低位移跟踪误差。

并联机械手集成电液伺服系统同步控制研究

为了提高并联机械手集成电液伺服驱动系统控制反应速度,降低末端执行器输出误差。介绍了一种具有三个独立控制的集成电液伺服驱动器,利用并联机械手的逆向运动学的表达式,推导出集成电液伺服驱动的平移并联机械手动力学模型。利用两个独立离散PI和PD控制器控制并联机械手输出力和位置,使驱动并联机械手三个液压缸输入电压控制信号保持同步。通过控制系统仿真软件对液压缸电压输入信号和末端执行器位置输出结果进行仿真。结果显示:采用同步控制方法,并联机械手集成电液伺服系统电压输入控制信号和末端执行器位置跟踪误差较小。采用同步控制方法,可以提高并联机械手集成电液伺服系统的自适应调节速度,提高末端执行器轨迹跟踪精度。

超重力下粒子图像测速系统性能测试与评价

粒子图像测速(PIV)技术作为一种无扰、瞬态、全速度场的测量手段,能够测量试验过程中土体的位移场变化、土体的瞬时运动速度等,具有传统的点或线式测量手段不具备的优势,近年来,已被推广应用于岩土工程离心模型试验中。然而,离心超重力的极端环境使PIV系统测速的准确性面临严峻考验。通过自行设计的一套可在超重力下提供稳定速度场的伺服调速标定装置,并以该装置提供的速度场为基准,对一套PIV系统在不同离心加速度、基准速度以及拍摄模式下的测速误差进行了测试和分析。研究结果显示:PIV系统的测速误差主要源自系统自身的时序控制误差,在50g离心加速度内,g值对系统性能的影响有限,常重力下测试结果提出的速度修正式同样适用于超重力工况;PIV系统的测试精度与相机的工作模式相关,连续拍摄时,两幅图像间隔时间越短,测试数据的离散程度越低;双曝光工作模式测试的数据点更为集中,系统精度更高;在像场的不同区域,PIV系统均能保持较小的系统误差和变异系数,能够实现全域测量。本研究为超重力条件下PIV技术的应用提供了可靠的校准方法,也为其他PIV系统的超重力性能测试与评价提供了参考。