高校体育多媒体教学平台系统的建设研究

本文从当前高校体育教学的周期短、学时少、教学方法单一的特点出发,充分的利用现代计算机网路多媒体技术,设计一套符合高校体育教育的多媒体教学平台系统,以满足学生课余时间的自主学习,增加教学的延伸性、娱乐性,为高校体育教育目标的实现提供保障。     

基于自适应修正曼哈顿距离的室内定位方法

在室内WiFi环境下,针对常见指纹匹配算法所忽略的信号波动问题,提出了一种基于自适应修正曼哈顿距离和AP选择的指纹匹配算法,并结合加权K近邻方法实现定位。首先采用AP选择算法获取部分受干扰程度小和出现频率高的AP,在指纹匹配时仅使用该部分AP的接收信号强度进行计算;在分析WiFi信号传播衰减公式和信号波动的基础上,提出了将自适应修正曼哈顿距离作为指纹匹配的度量距离,使用该距离旨在平滑信号波动对指纹相似度计算的影响;最后采用加权K近邻方法估计测试点的坐标。实验结果表明,在加权K近邻方法的框架下,基于自适应修正曼哈顿距离的定位算法在定位精度上优于基于欧氏距离、曼哈顿距离、余弦距离和Sorensen距离的定位算法。     

IET短周期涡轮实验台

本文介绍了中国科学院工程热物理研究所（IED最新建成的暂冲式短周期涡轮实验台的装置结构和关键设备的研制原理及性能，描述了短周期涡轮实验过程、实验台的控制系统和测试系统，展示了本实验台的部分标志性实验结果。实验结果表明：实验台的建造是成功的，充分体现了短周期实验的长处，对验证和发展涡轮的设计与计算具有实际应用价值。     

Control law design for transonic aeroservoelasticity

Existing computational transonic aeroservoelastic researches focus on directly coupling the structural dynamic equations, CFD solver and servo system in time domain, study the effect of the given feedback control laws on the responses of the aeroelastic system. These works have not involved the design of the flutter active control law. The non-linearity of transonic flow brings great difficulties to aeroservoelastic analysis and design. Recent research of the unsteady aerodynamic reduced order models (ROM) based on CFD provides a challenging approach for transonic aeroservoelastic analysis and design. Coupling the structural state equations with the aerodynamic state equations of the wing and the control surface based on the ROM, we construct a transonic aeroservoelastic model in state-space. Then the sub-optimal control method based on output feedback is used to design the flutter suppressing law. The study first demonstrates the open loop of the Benchmark Active Controls Technology (BACT) wing. The computational results of the CFD direct simulation method and the ROM analysis method are both agree well with the experimental data. Then both the closed loop time responses and the flutter results by ROM technique are compared with those of numerical aeroservoelastic simulation based on Euler codes to validate the correctness of the design method of the control law and aeroservoelastic analysis method. An increase of up to 20% of the speed index can be achieved by the control law designed by sub-optimal control method for this model.     

并联磨床加工螺旋槽的磨削参数设计

螺旋槽的加工是回转体刀具加工的重要组成部分,其形状参数(尤其是前角、槽深和槽宽)对刀具的切削过程有很大的影响.基于6-UPS并联机床,在分析并联机床加工工艺特性的基础上,按照螺旋槽加工中砂轮与刀具的相对运动关系,建立了螺旋槽加工运动的理论模型,对可能影响螺旋槽成形的因素进行了全面分析.进而建立了一个仿真模型,可以对所有的磨削参数进行快速的定量设计和优化,主要包括砂轮偏转角度、砂轮厚度、砂轮轴向平移位置和螺旋槽深度,并通过加工实验进行了验证.     

民航VHF地空通信干扰对策研究

民航VHF地空通信干扰是近年来困扰中国民航的难点问题。通过对中国某机场干扰情况的深入调查和研究，明确了主要干扰源及其产生机理。同时结合中国电磁环境的实际情况和民航自身的特点，提出了从民航自身入手、加强管理、建立监控体系和应急VHF通信接收系统的解决思路。     

PANIC – A surface science package for the in situ characterization of a near-Earth asteroid

This paper presents the results of a mission concept study for an autonomous micro-scale surface lander also referred to as PANIC – the Pico Autonomous Near-Earth Asteroid In Situ Characterizer. The lander is based on the shape of a regular tetrahedron with an edge length of 35 cm, has a total mass of approximately 12 kg and utilizes hopping as a locomotion mechanism in microgravity. PANIC houses four scientific instruments in its proposed baseline configuration which enable the in situ characterization of an asteroid. It is carried by an interplanetary probe to its target and released to the surface after rendezvous. Detailed estimates of all critical subsystem parameters were derived to demonstrate the feasibility of this concept. The study illustrates that a small, simple landing element is a viable alternative to complex traditional lander concepts, adding a significant science return to any near-Earth asteroid (NEA) mission while meeting tight mass budget constraints.     

Damage tolerance of composite structures for large transport aircraft

Damage of composite materials is studied at a coupon level from both a fracture mechanics and a damage mechanics point of view. Methods developed are applied to sub-elements and sub-structures with the objective of decreasing the amount of testing needed in the certification procedures of composite structures.     

实现Developer/2000环境下动态生成报表功能

通常数据库应用系统中的输出报表必须在系统开发阶段定制,不能满足用户不断变化的管理需求.介绍了用Oracle开发工具Developer/2000结合DDE(Dynamic Data Exchange)技术实现任选查询和动态生成报表的方法,这种方法允许用户根据自己的要求选择输出报表的内容和格式,并利用Excel进行编辑,极大地增强了系统的报表生成能力和灵活性,具有很好的实用性.      

前向神经网络快速学习算法在发动机模型辨识中的应用

介绍一种采用前向神经网络辨识发动机非线性模型的快速学习方法,与现有同类方法相比,该方法采用矩阵的QR分解求解线性方程组,解决了维数过高的矩阵直接求逆带来的解失真问题,并把这种方法应用于航空发动机的非线性模型辨识。算例仿真验证了算法的可行性。