摘要：Blades are one of the important components on aircraft *** they break due to vibration failure,the normal operation of the entire engine will be ***,it is necessary to measure their natural frequency before installing them on the engine to avoid *** present,most blade vibration testing systems require manual operation by operators,which has high requirements for operators and the testing process is also very ***,the testing efficiency is low and cannot meet the needs of efficient *** solve the current problems of low testing efficiency and high operational requirements,a high-precision and high-efficiency automatic test system is *** testing accuracy of this system can reach ±1%,and the testing efficiency is improved by 37% compared to manual ***,the influence of compression force and vibration exciter position on natural frequency test is analyzed by amplitude-frequency curve,so as to calibrate servo cylinder and fourdimensional motion ***,the sine wave signal is used as the excitation to sweep the blade linearly,and the natural frequency is determined by the amplitude peak in the frequency ***,the accuracy experiment and efficiency experiment are carried out on the developed test system,whose results verify its high efficiency and high precision.

摘要：跟踪注册是增强现实(Augmented reality,AR)中一项至关重要的技术。基于人工标识和基于图像的注册方法已广泛应用于增强装配系统中。然而,由于空间产品的弱纹理、结构对称、数据有限以及难以张贴标识等特点,空间站的跟踪注册仍面临挑战。本文提出了一种专门为中国空间站诱导维修应用设计的三维物体跟踪方法,旨在用AR技术取代传统的纸质手册,为宇航员提供更直观的操作指导。本文提出了一种无标记的中国空间站智能维护方法。采用点对特征方法来估计初始帧姿态,不需要手动调整来获得相应的姿态,这对宇航员来说至关重要,因为在微重力环境中精确运动是一项重大挑战,而且结合曲率信息可以提高采用点对特征方法估计初始帧姿态的效率。通过结合纹理和区域信息,消除了对宇航员位置的精确限制,进一步增强了空间对称产品的跟踪鲁棒性。该方法利用点云匹配来估计第一帧的初始姿态,并在失去跟踪后重新计算姿态。一旦获得了前一帧的姿态,则仅根据二维图像的区域和纹理信息来计算跟踪,以获得实时跟踪。实验结果表明:本文方法与基于标识的方法具有相同的姿态趋势;基于电子游标卡尺测量之间的误差在毫米级;使用专门为航天产品设计的专用工具成功更换过滤器,证明了在空间站上实施诱导维修程序的实用性和潜力。

摘要：成功实现高转换效率的140 GHz TE22,6准光模式变换器原型设计。基于周期微扰原理设计Denisov辐射器,实现低边缘绕射的初级出射波束。针对三镜面光路系统,采用全矢物理光学积分作为主要计算手段,围绕主极化场分量进行三级相位修正面迭代优化,实现高出射高斯纯度的模式场转换,其中一级镜的修正有效改善了辐射器出射的不理想性。基于全矢数值仿真确认,相比原二次曲面原型设计,相位修正后的变换器系统的出射高斯纯度从92.7%提高到99.6%,结合98.8%以上的功率传递效率,实现了性能优越的高阶回旋管准光模式变换器原型设计。

摘要：以飞机电动环控用高速永磁同步电机(High-speed permanent magnet synchronous motor,HSPMSM)控制系统为研究对象,考虑到HSPMSM无传感器控制的研究主要集中在算法实现和转子估计误差消除方面,本文提出了一种基于小信号分析的无传感器全速控制全局稳定性分析和参数设计方法。该方法在扩展反电动势法的基础上设计了位置估计环的参数,并建立了位置估计环和速度环的参数对系统稳定性的影响。其次,本文使用根轨迹来设计I/f控制能够运行的最高转速和扩展反电动势法能够运行的最低转速,以确定算法切换的稳定转速。同时分析了电机参数在高温下的灵敏度。最后,在45 kW、4000 r/min表贴式HSPMSM上进行了全速域电动环控实验。结果表明,本文设计的回路参数和切换转速具有更好的动态和稳态性能,参数的灵敏度与理论分析一致,为HSPMSM的全局参数设计和灵敏度分析提供了可行的思路。

摘要：A conformal optical system refers to the one whose first optical surface conforms to both aerodynamic and imaging requirements. Appropriate correction is required because a conformal dome induces significant aberrations. This paper intends to explain that an effective solution to the easy-fabrication conic surface corrector compensates aberrations induced by a coaxial aspheric dome. A conformal optical system with an ellipsoid MgF2 conformal dome, which has a fineness ratio of 2.0, is designed as an example. The field of regard angle is -4-30 degrees with a ＋2 degree instantaneous field of view. The system＇s ultimate value of modulation transfer function is close to the diffraction limit, which indicates that the performance of the conic conformal optical system with a fixed conic corrector meets the imaging requirements.

摘要：机器视觉经济高效,在焊缝检测中得到广泛的应用。基于线结构光技术,本文提出一种坡口特征尺寸检测方法。首先,针对激光光条灰度和宽度分布不均的问题,介绍了一种基于二次加权灰度重心法的自适应中心线提取算法。其次,为滤除图像噪声,设计了一种基于感兴趣区域划分和图像差分的预处理算法。接着,本文提出了一种亚像素特征点提取算法以计算坡口特征尺寸并识别坡口类型。最后,实验结果表明,坡口特征尺寸检测的绝对误差为0.031~0.176 mm,相对误差为0.2%~3.6%。

摘要：During airdrop of heavy load, the flight parameters vary continuously as the load moves in the hold, and change suddenly when the load drops out. This process deteriorates the flight quality and control characteristic as the load becomes heavier. Based on the simplified airdrop flight equations, the backstepping and switch control methods are developed to tackle the flight state holding and disturbance/uncertainty （such as large-scale flight condition, pilot manipulation error, system measure delay, etc.） attenuation problem in this paper. Moreover, these methods can be used as a reference for pilot manipulating during airdrop. With the backstepping theory, an adaptive controller is synthesized moves in the hold, and then a coordinated switch control method is for the purpose of stabilizing the transport when the load used to control the aircraft when the condition jumps from the existence of load at the rear of fuselage to no load in the fuselage. Simulation results show that the proposed controllers not only provide effective state holding during airdrop, but also achieve robust performance within wide flight conditions.

摘要：In this paper, we present an efficient method to obtain absorbers with broadened operating frequency bands. They are accomplished by using conventional magnetic absorbing materials （MAMs） in the forms of array and mesh structures, which are similar to those in the case of a frequency selective surface. The proposed approach is verified not only by simulations but also by experimental results under the normal incidence at microwave frequencies. Moreover, the wideband absorber is lighter than the conventional magnetic absorber. These results indicate that our proposed absorbing structures can be used for designing good electromagnetic absorbers.

摘要：In this paper, a novel approach is proposed for solving the parameter design problem of brushless direct current(BLDC) motor, which is based on the membrane computing(MC) and pigeon-inspired optimization(PIO) algorithm. The motor parameter design problem is converted to an optimization problem with five design parameters and six constraints. The PIO algorithm is introduced into the framework of MC for improving the global convergence performance. The hybrid algorithm can improve the population diversity with better searching efficiency. Comparative simulations are conducted, and comparative results are given to show the feasibility and effectiveness of our proposed hybrid algorithm for high nonlinear optimization problems.

摘要：零泊松比(Zero Poisson’s ratio,ZPR)胞状结构等智能结构因其重量轻、有效模量低的突出特点,在变形翼等领域的应用逐渐兴起。本文研究了ZPR胞状结构的面内和面外力学性能,提出了计算ZPR胞状结构的面内拉伸模量、面内剪切模量和面外弯曲模量的理论方法,分析了蜂窝结构几何构型对其面内、面外力学性能的影响。在有限元模拟的基础上,系统地研究了面内拉伸、剪切模量和面外弯曲模量。实验验证了理论分析和有限元分析的可行性和有效性。结果同时表明,通过设计胞体几何参数可以控制ZPR胞状结构的面内和面外力学。