宿舍管理中心管理信息系统的开发

本文主要介绍宿舍管理中心管理信息系统的分析、设计、实现、维护的整个过程,特别强调了系统分析设计、数据库设计思路。     

方坯叶片电解加工过程的模糊控制方法

采集方料毛坯叶片电解加工整个过程的电流信号,用小波变换法对信号进行降噪处理,得到一条电流随间隙减小而呈增大趋势的光滑曲线。设计了一种二维M andan i型模糊控制器,以所得光滑电流曲线作为标准曲线,以加工电压的增量为模糊控制器输出,控制实际加工电流,使其在多种扰动下跟踪标准电流曲线。在M atlab的S im u link模块中,通过对由模糊控制器和电解加工系统组成的联合模型进行仿真试验,整定模糊控制器的3个增益参数。仿真试验表明,该方法可使电解加工系统较好地重现预设的加工过程,实现对电解加工全过程的控制。该方法也可以应用于其他类型的电解加工过程控制。     

Separation process of multi-spheres in hypersonic flow

The separation process of multi-spheres in hypersonic flow has been experimentally investigated. The experiments were conducted in a shock tunnel at a nominal freestream Mach number of 6. Iron or acetal small light spheres with different sizes, varying from 2.38 to 6 mm, were considered. They were mounted by a thin wire. The trajectory of the spheres was analyzed using optical images. By varying the radius and the number of spheres from a single to multiple spheres, the lateral velocity and the separation behavior including the phenomenon known as ‘shock wave surfing’ were measured and analyzed. A new equation to account for the lateral velocity of the multi-spheres was proposed by extending the well-known Passey and Melosh’s theory based on two bodies. The theoretical results were compared with the presented experimental data and a good agreement was found. Using the derived equation, the re-entry trajectory analysis of multi-spheres, that is regarded as the hypothetical break-up, was performed. The ground footprint and downrange due to the separation of the multi-spheres were compared with that of single- and two-spheres. The results showed that as the number of spheres increased, the lateral velocity increased while the ballistic coefficient decreased. This led to a large discrepancy in the ground footprint as well as the downrange when compared to the single sphere. Caution should therefore be exercised in the trajectory analysis when the effect of separation induced due to fragmentation is not considered.     

相控阵雷达长时跟踪波束调度与波形优化策略

针对相控阵雷达多目标跟踪波束调度和波形参数优化控制的问题，本文提出了一种基于马尔可夫决策过程（MDP）的相控阵雷达跟踪波束调度与波形参数优化策略，该方法以无迹卡尔曼滤波（UKF）算法为基础来估计目标的状态。首先将本文的序列决策问题建模为马尔可夫决策过程，定义了资源的效费比和长期回报率，然后与当前实际跟踪误差综合考虑作为MDP的回报函数，进而给出了调度的优化模型，最后将长时决策问题转化为动态规划算法结构进行求解，并且提出了一种并行混合遗传粒子群优化算法来求解各决策时刻的最优策略。仿真结果表明了长时策略的先进性以及寻优算法的优越性，与传统的短时策略相比，跟踪精度可提高11.17%。     

基于位姿测量不确定度的飞机对接质量评估

针对基于位姿的数字化测量辅助飞机大部件对接技术的发展与应用,对位姿测量不确定度以及基于不确定度的质量评价方法进行了研究.给出了数字化对接环境下大部件位姿的数学表达形式及意义.提出了基于协方差矩阵的位姿测量不确定度解析算法,并通过仿真算例与蒙特卡洛仿真法进行了对比,验证了该算法的有效性.给出了飞机大部件对接过程数字化测量工艺能力指数的概念,用于对测量结果的可信性进行评价;通过构建位姿测量不确定度与对接质量评估指标间的映射关系,提出了一种基于位姿测量不确定度的大部件对接质量评估方法,并以机翼-机身对接过程为案例,对方法的可行性、算法的有效性进行了验证.     

MEMS技术中的电镀工艺及其应用

电镀已经成为MEMS(Micro-Electro-Mechanical System)技术中的一种重要加工手段,相比于传统意义的表面处理作用,MEMS技术中的电镀主要用于制作微结构.介绍了几种常用的以电镀为核心方法的微结构加工工艺和它们的应用领域.微结构加工工艺包括LIGA/UV-LIGA、EFAB、PolyStrat...     

波音757客改货15货盘的L1门区域改装

L1门区域改装是波音757-200客改货工作的核心内容,本文简要介绍了进行波音757-200客改货(15个货盘改装方案)L1门区域改装中所采用的的工作方法。     

不同热处理工艺下激光增材制造TC4钛合金组织与性能研究进展

由于激光增材制造(Laser Additive Manufacturing,LAM)TC4钛合金加工成形过程的特殊性,导致该合金在力学性能上存在明显的各向异性,同时韧性、疲劳性能不能很好地满足使用要求。从材料组织与力学性能之间的关系出发,介绍了不同热处理工艺对激光增材制造TC4钛合金组织与力学性能的影响,指出了当前激光增材制造TC4钛合金热处理研究中存在的问题,并为后续激光增材制造TC4钛合金的热处理研究提供思路与方向。     

周边封闭铝蜂窝夹层结构配合改进和胶接工艺研究

采用多种材料作为校验膜测试零件间的配合间隙,分析对比使用效果确定了最佳校验材料。对柔性蜂窝芯零件的周边加强和定位进行了研究,在蜂窝芯边缘和倒角区采用泡沫胶修形,改善零件间的配合关系。为提高板_板区的胶接质量,采用自制压条使板_板胶接区平整,且满足了无损检测的要求。     

Sunspot cycle prediction using Warped Gaussian process regression

Solar cycle prediction is a key activity in space weather research. Several techniques have been employed in recent decades in order to try to forecast the next sunspot-cycle maxima and time. In this work, the Gaussian process, a machine-learning technique, is used to make a prediction for the solar cycle 25 based on the annual sunspot number 2.0 data from 1700 to 2018. A variation known as Warped Gaussian process is employed in order to deal with the non-negativity constraint and asymmetrical data distribution. Tests using holdout data yielded a root mean square error of 10.0 within 5 years and 25.0–35.0 within 10 years. Simulations using the predictive distribution were performed to account for the uncertainty in the prediction. Cycle 25 is expected to last from 2019 to 2029, with a peak sunspot number about 117 (110 by the median) occurring most likely in 2024. Thus our method predicts that solar Cycle 25 will be weaker than previous ones, implying a continuing trend of declining solar activity as observed in the past two cycles.