基于复杂网络的航空制造供应链关键节点识别研究

随着不稳定因素的增加以及航空制造供应链的参与主体增多，航空制造供应链的管理所面临的风险也随之增大。因此针对航空制造供应链网络的风险管理，以复杂网络为工具研究供应链网络中的关键节点识别问题，从而帮助航空供应链提升抗风险能力。通过分析我国航空制造供应链网络现状和特点，提出供应链形成机制并划分供应链层级，对航空制造供应链进行构建及指标界定，对度中心性、介数中心性、接近中心性三种经典中心性算法以及传统K-Shell 分解算法进行加权改进；结合熵值-TOPSIS 法提出一种针对加权网络的供应链关键节点识别算法——WKC 算法，通过构造网络来进行算例分析，验证该种算法的有效性。结果表明：本文提出的WKC 算法原理科学、计算复杂度较低，为航空制造等高端装备制造业供应链的风险管理提供了一定的参考。     

变截面悬臂梁结构动载荷辨识方法

在航空航天领域，作用在结构上动载荷的确定对结构健康监测是非常必要和重要的。为此，本文以类似机翼结构的变截面悬臂梁结构为研究对象，提出了一种基于光纤光栅传感器与卡尔曼滤波器的动载荷识别方法。首先，根据变截面梁单元形式，推导出变截面梁的质量矩阵与刚度矩阵，建立动力学运动方程。然后，以光纤光栅传感器测得的应变信息作为观测信号，通过卡尔曼滤波器生成的增益矩阵、新息序列矩阵以及协方差矩阵，得到灵敏度矩阵和估计力的增益矩阵。在此基础上，利用广义回归模型及其最小二乘算法，估算出动载荷大小、判断出动载荷激励位置。借助数值仿真与实验手段，分别验证了该方法对于单点正弦激励、方波激励、锯齿波激励以及多点同时激励等工况下的动载荷识别效果。结果表明，本文所提算法具有较好的动载荷识别效果和噪声抑制能力，能够为未来风洞试验和真实飞行试验环境中诸如大展弦比机翼表面气动压力等载荷实时辨识、气动外形自适应控制以及结构健康监测提供技术支撑。     

Boundary condition modelling and identification for cantilever-like structures using natural frequencies

The actual boundary conditions of cantilever-like structures might be non-ideally clamped in engineering practice, and they can also vary with time due to damage or aging. Precise modelling of boundary conditions, in which both the boundary stiffness and the boundary mass should be modelled correctly, might be one of the most significant aspects in dynamic analysis and testing for such structures. However, only the boundary stiffness was considered in the most existing methods. In this paper, a boundary condition modelling and identification method for cantilever-like structures is proposed to precisely model both the boundary stiffness and the boundary mass using sensitivity analysis of natural frequencies. The boundary conditions of a cantilever-like structure can be parameterized by constant mass, constant rotational inertia,constant translational stiffness, and constant rotational stiffness. The relationship between natural frequencies and boundary parameters is deduced according to the vibration equation for the lateral vibration of a non-uniform beam. Then, an iterative identification formulation is established using the sensitivity analysis of natural frequencies with respect to the boundary parameters. The regularization technique is also used to solve the potential ill-posed problem in the identification procedure.Numerical simulations and experiments are performed to validate the feasibility and accuracy of the proposed method. Results show that the proposed method can be utilized to precisely model the boundary parameters of a cantilever-like structure.     

基于过程方法的测量设备控制

测量设备控制是企业内部管理和外部质量管理体系审核中的一项重要内容,在现有的管理中,因缺乏对相关过程进行系统识别,某些过程要素常被疏忽或遗漏,导致测量设备失控和测量结果失准。本文采用过程方法,系统地识别了测量设备控制的相关过程和过程要素,提出了过程监控指标及其评价准则,对于提高过程效率具有一定的参考价值。     

基于随机时隙的RFID读写器防冲突方法

针对密集读写器环境下的无线射频识别(RFID,Radio Frequency Identification)多读写器冲突情况,提出了一种基于随机时隙并通过中央计算机协调的读写器防冲突方法.首先,中央计算机发送每轮起始命令和时隙指令,读写器根据当前利用率随机选择时隙.选择当前时隙的读写器若没有接收到忙信号则发送信标并侦听,若无邻近读写器发送信标则开始读写标签,否则该轮回停止工作.若时隙末存在没有接收到忙信号的读写器则在额外时隙发送二次信标.与现有的分布式防冲突方法相比,该方法具有较好的吞吐量和公平性.     

加速度计温控系统被控对象建模技术研究

加速度计工作过程中,其内部与外界环境存在温度梯度,针对温度变化影响加速度计参数的问题,提出了一种加速度计温控系统被控对象建模的方法。进行了多工作点加速度计升温和降温试验,采用递推增广最小二乘法对被控对象模型进行了辨识,建立了加速度计温控系统被控对象模型和降温模型,计算结果表明,3min后温控系统被控对象模型曲线残差在-0.5~0.5℃之间,降温模型曲线残差在-0.15~0.15℃之间,满足系统对加速度计性能需求,表明了方法的有效性。     

氨合成-水热改性法制备氢氧化镁阻燃剂

为了解决氢氧化镁和聚合物之间的不相容问题, 对氨合成法-水热改性处理2步法制备高分散氢氧化镁阻燃剂进行了研究,分析了常温合成温度、水热改性温度和水热改性时间对制备大晶型、低比表面积氢氧化镁阻燃剂的影响.结果表明,经过水热改性处理改变了氢氧化镁晶体的生长习性,生成了形貌规则、粒径分布均匀、分散性良好的氢氧化镁六方片状颗粒.另外通过提高氯化镁浓度和氨水过量1倍,探讨了常温合成反应的转化率,认为应该在反应原料等当量下寻求提高转化率的可行方法.     

辐射源细微特征用于个体识别的可行性分析

首先分析了辐射源细微特征应该具有的基本特性,并给出了辐射源的(潜在)细微特征参量、测量准确度的影响因素及应用限制条件.然后,给出了辐射源细微特征差异、参数测量精度与正确分辨概率之间的定量关系,为判断细微特征差异能否用于个体识别提供了理论依据.最后,作了举例说明.     

High-efficiency aircraft antiskid brake control algorithm via runway condition identification based on an on-off valve array

The aircraft antiskid braking system is an important hydraulic system for preventing tire bursts and ensuring safe take-off and landing. The brake system adjusts the force applied on the brake discs by controlling the brake pressure. Traditional aircraft antiskid braking systems achieve antiskid performance by controlling the braking pressure with an electrohydraulic servo valve. Because the pilot stage of an electrohydraulic servo valve is easily blocked by carbonized hydraulic oil, the servo valve would become a dangerous weak point for aircraft safety. This paper proposes a new approach that uses an on-off valve array to replace the servo valve for pressure control. Based on this new pressure control component, an efficient antiskid control algorithm that can utilize this discontinuous feature is proposed. Furthermore, the algorithm has the ability to identify the runway circumstances. To overcome the discontinuity in the process of using an on-off valve array, the Filippov framework is introduced. The conditions of convergence of the system are also discussed. The results of the digital simulations and the hardware-in-the-loop (HIL) braking experiments are used to verify the efficiency and stability of the proposed control algorithm. The method also proves that the on-off valve array can replace the servo valve perfectly as a new type of antiskid braking pressure control component.     

高阶矩谱分析与空间等离子体非线性相互作用识别

利用高阶矩统计分析方法对ＡＵＲＥＯＬ－３卫星观测数据进行分析处理，所涉及的信号分别为ＥＬＦ频率范围内的电场扰动Ｅｈ（ｔ）和等离子体密度波动δＮｅ／ｎｅ（ｔ），处理结果表明：利用高阶矩谱分析方法可以很好地识别空间等离了波－粒相互作用过程中的非线性成分