高职物流教育存在的问题及解决对策

通过分析我国高职物流教育的现状及存在的培养目标定位模糊、师资缺乏、教材质量差、教学手段和方法单一等问题。提出了明确培养目标、加强师资队伍和教材建设、改革教学方法等对策。阐述了只有更新观念，不断创新，高职院校才能为我国物流行业培育出更多高素质的适用人才。     

应用信标模式测速的实现方法及论证

根据未来固体火箭型号试验越来越多,首区无线电设备受火箭尾焰干扰的情况以及测控体制的发展要求,探讨了利用信标模式[1]进行高精度测量时所面临的工程问题,包括信标模式下测量值的误差项分析,减小测量误差的方法等内容。     

现代企业的成本管理研究

本分析了现代企业的特征和传统成本管理模式存在的弊端,提出了现代企业成本管理的构想,即建立以“作业”为基础的成本管理新模式。现代企业的成本管理以“作业”为基础进行管理,就是将作业消耗资源和产品消耗作业有机的结合在一起,确定目标成本,控制与管理成本。高新科学技术越发达,成本管理越重要。     

基于多媒体计算机英语电影教学的实验研究

从对多媒体计算机英语电影教学,在听说教学过程中进行的实验结果表明:英语电影教学对学生的英语学习成绩和各项能力的提高有很大的影响,正式开设英语电影课程很有必要。     

Efficient computation of energy release rates for delaminated beam structures

The often encountered problem of mode partitioning for delaminated, isotropic beam structures is addressed. For the sake of efficiency, solutions that do not require complex continuum solutions – in practise mostly obtained by the finite element method – are examined. Three approaches that meet the postulated efficiency are reviewed and compared. While one method fits consistently into the concept of linear-elastic fracture mechanics, the remaining two deduce mode partitioning hypotheses solely from kinematic quantities of beam theory. The results obtained through these hypotheses are then compared to continuum-based solutions. The latter are generated by the finite element method and are validated by analytical solutions as applicable. Furthermore, mode partitioning solutions for beams, loaded in transverse shear, are given with excellent accuracy. Finally, the conditions for which the different methods comply with or substantially deviate from each other are discussed.     

利用EMD方法提取太阳活动周期成分

EMD(经验模态分解)方法在处理非线性及非平稳时间序列时表现出了很大的优势和应用潜力.利用EMD方法研究太阳活动周期,对110年(1894-2003)和55年(1949-2003)的太阳黑子数月均值进行分解,分别得到一系列模式和一个趋势项,其中都可能包含有1.3至1.4年周期分量,25至30个月QBO(准双年振荡)分量,11年太阳周分量和22年Hale周分量.其中11年周期分量幅度最大,变化特征与太阳黑子数原始数据具有很高的相似性.不同于传统方法,EMD方法给出了太阳活动在不同时间尺度上各自分离的变化特征.      

硬X射线调制望远镜(HXMT)天文卫星的结构分析

根据HXMT卫星的结构形式,建立卫星的有限元模型,进行静力、模态、频率响应计算,得出了最大纵向、最大横向过载联合作用下卫星各组成部分的最大应力值.对整星结构进行了模态计算和频率响应分析,得出了100Hz以内的模态频率值.结合理论分析和以往的设计经验,提出了对该卫星结构的合理改进建议.      

Two-phase guidance law for impact time control under physical constraints

An impact-time-control guidance law is required for the simultaneous attack of suicide attack unmanned aerial vehicles. Based on the nonlinear model, a two-phase guidance strategy is proposed. The impact time is derived in a simple analytical form of initial states and switching states, and it can be controlled by switching at an appropriate range. Firstly, a two-phase guidance law is designed to make the magnitude of the heading error decrease monotonically from its initial value to zero. And then, the feasible interval of the switching ranges and of the impact times under the acceleration constraint are given analytically in sequence. Furthermore, a general form of two-phase guidance law is proposed, which allows the magnitude of the heading error to increase in the first phase, to improve the applicability of the methodology. Having the same structure as proportional navigation guidance with a time-varying gain, the proposed algorithms are simple and easy to implement. The corresponding feedback form is presented for realistic implementation. When a predefined impact time is taken within its permissible set, the constraints on the acceleration and field-of-view will not be violated during the interception. Finally, simulations validate the effectiveness of the methodology in impact time control and salvo attack.     

关于重型运载火箭若干问题的思考

重型运载火箭涉及众多关键技术,研制难度大,研制周期长。针对重型运载火箭研制过程中的几个问题进行了思考,包括动力类型选择、重型火箭模态试验、动力系统试车、测发模式以及产业基地布局与建设等方面,提出重型运载火箭后续研制过程中的技术难点以及应对措施设想。     

基于振型节径谱的失谐叶盘结构动态特性评价

基于叶盘结构振型的离散傅里叶变换,给出振型节径谱的定义。对于一个简化的叶盘结构,利用节径谱的概念对失谐叶盘的动态特性进行了评价和分析。在固有特性方面,基于节径谱改进了模态局部化因子的定义,得到了随机失谐叶盘的模态特性的统计特征;在响应特性方面,基于振型和激励节径谱的相似程度定义了模态激励因子,很好地解释了随机失谐程度的＂阈值＂效应和最优人为失谐的存在性。算例表明,节径谱是衡量的振型空间分布的重要指标,在失谐叶盘结构动态特性分析和评价中有着重要的应用。