Real-time translational control of a MEMS comb resonator

Closed-loop control has been successfully applied to a microelectromechanical systems (MEMS) lateral comb resonator device in real-time to perform impulse disturbance damping and sinusoidal position control, enabled by the use of a through-wafer optical microprobe to obtain position feedback. This result leverages the application of lifetime, in-situ control of MEMS in order to provide quality assurance of microsystems in safety critical applications. A position feedback signal produced by a through-wafer optical microprobe has been used for comb resonator system model identification by two independent methods to accurately determine the effective mass, damping, and spring constant values of the device. After accurate determination of system parameters, closed-loop impulse disturbance damping and proportional-integral-differential (PID) translational control were applied. Closed-loop control results presented indicate controllability of such microstructures and response times on the order of the natural frequency of the device.     

Experimental study of damping properties of a composite torsion bar in the helicopter main rotor hingeless hub

The results of the experimental studies of damping characteristics of a composite torsion bar in the helicopter main rotor hingeless hub are presented. A variant of their improvement is considered.     

The finite element analysis of shells of revolution with a branching meridian

We present an algorithm for calculating the shells of revolution with the branching meridian using the triangular finite elements, the rigidity matrices of which are formed based on the vector method of displacement interpolation [1]. The correct kinematic and static conditions of shell conjugation on the line of their coupling have been developed. The shell structure consisting of a cylinder and adjacent shells is calculated under various conditions of support.     

基于ADAMS/Aircraft的起落架滑跑模型仿真

以小车式起落架为例,利用ADAMS/Airc- raft建立了起落架滑跑试验仿真模型.给出了起落架滑跑运动方程,并进行了滑跑试验仿真分析。仿真结果与理论要求对比具有较好的一致性。     

最坏风模型及对飞机突防航迹跟踪的影响

针对一类非线性动力学系统,本文推导出二次型性能指标下的微分对策解,由此得到一组含有非线性因素的最环风模型,这一模型特别适用于研究作空间机动飞行的飞机受外界环境扰动的灵敏性问题。最后考察了这一变化风场对飞机突防航迹非线性解耦跟踪的影响。     

用集成功放组成的精密功率放大器

介绍了一种用厚膜集成功放加上稳幅电路组成的精密功率放大器，其稳定度、频率响应和波形失真都达到了很高的指标。     

万工显滑板移动直线度的检修

通过对影响万能工具显微镜滑板移动直线度的分析 ,提出有针对性的修理方法 ,并分别论述了产生线值偏差和角度偏差的主要原因。     

新型精密狭缝的设计

介绍了一种基于弹性铰链的精密狭缝的设计，加工工艺要求和性能测试结果。根据实际需要，狭缝可以采用水冷结构。     

CC—高阶通信系统的并发演算

并发演算CC(Concurrent Calculus)是高阶并发通信系统的数学模型,它把λ-演算作为子理论并包含一阶通信系统演算CCS、活动进程演算CMP、和高阶通信系统演算CHOCS的主要特征。在CC中,通信端口可为任意表达式并且进程和通信端口都可以作为在通信中传递的一等对象(First-class Objects)。从而CC不仅可以描述一阶通信行为而且可以刻划通信网络的动态自修改行为。另外,由于CC把λ-演算和进程演算纳入同一形式系统,故CC可以作为并发函数式程序设计的核心语言和理论模型。本文首先给出CC的语法、语义和例子,然后研究CC的高阶双向模拟等价关系以及CC的代数定律。最后简单讨论了相关的工作和今后的研究方向。     

含有任意多个椭圆孔弹性板的应力场计算

本文应用弹性力学的复变函数理论,用多保角变换的方法,导出了含有任意多个椭圆孔的无限大弹性板多复变量应力函数的表达式。每个孔的大小、位置和孔边作用的载荷均为任意指定。板的无限远处作用有和坐标轴方向一致的均匀拉压载荷P_x,P_y和均匀剪切载荷P_(xy)。并在孔边进行复Fourier级数展开,用待定系数法确定应力函数的未知系数,从而计算弹性板的应力场。编制了相应的FORTRAN77标准化程序,进行了考题和算例分析,给出了级数的收敛状况和孔边周向应力的分布图。