单级跨声速压气机进气畸变数值模拟

基于彻体力模型的基本思想,发展了一套能够反映进气畸变对风扇/压气机气动性能影响的三维数值计算程序CSAC.首先详细研究了彻体力模型的具体建模方法,然后发展了相应的三维数值计算程序.利用该程序针对某单级跨声速压气机在均匀进气下的流场进行了计算验证,计算结果与雷诺平均Navier-Stokes(RANS)计算吻合得很好,流场主要参数分布与相关实验数据也有很好的一致性.利用该程序分别计算分析了进口存在稳态周向总压畸变及周向总温畸变的全环三维畸变流场,结果表明:压气机进口畸变流场存在大尺度、强三维特征,将导致压气机总压比及稳定裕度下降.所有计算结果均显示该模型能够在降低对计算资源和工程经验依赖的同时,有效分析进气畸变对压气机特性的影响.      

叶片脱落诱发的转子- 盘片系统不平衡响应分析

为了厘清叶片脱落诱发的失衡载荷及瞬时冲击对航空发动机转子系统动特性的影响,以转子- 盘片系统为研究对象, 考虑弹性支承的影响,基于ANSYS/LS-DYNA 软件建立系统的有限元模型,模拟叶片脱落对转子- 盘片系统振动响应的影响,分析转 子转速、不平衡量、盘偏置量及支承刚度对系统不平衡振动响应的影响规律。结果表明：轴承支承总反力的变化趋势与系统不平衡 量的变化趋势相同;盘片结构越靠近轴承支承端,轴承支承总反力越小;刚性支承（≥107 N/m）下轴承支承总反力较柔性支承（<107 N/m）下的偏大。该研究可为转子- 盘片系统的结构设计提供参考。     

航天器共因失效分析与预防初探

简要介绍了共因失效相关概念及分析方法,通过共因失效案例分析,对航天器如何开展共因失效分析以及如何预防共因失效进行了初步探讨,提出了航天器开展共因失效分析的定性和定量方法以及预防共因失效的措施。     

GNSS reflectometry and remote sensing: New objectives and results

The Global Navigation Satellite System (GNSS) has been a very powerful and important contributor to all scientific questions related to precise positioning on Earth’s surface, particularly as a mature technique in geodesy and geosciences. With the development of GNSS as a satellite microwave (L-band) technique, more and wider applications and new potentials are explored and utilized. The versatile and available GNSS signals can image the Earth’s surface environments as a new, highly precise, continuous, all-weather and near-real-time remote sensing tool. The refracted signals from GNSS radio occultation satellites together with ground GNSS observations can provide the high-resolution tropospheric water vapor, temperature and pressure, tropopause parameters and ionospheric total electron content (TEC) and electron density profile as well. The GNSS reflected signals from the ocean and land surface could determine the ocean height, wind speed and wind direction of ocean surface, soil moisture, ice and snow thickness. In this paper, GNSS remote sensing applications in the atmosphere, oceans, land and hydrology are presented as well as new objectives and results discussed.     

大学生就业报道的内容分析——以《中国青年报》为例

通过《中国青年报》关于大学生就业报道内容的分析,得出其立足点与政府立场和就业政策的高度一致,注重报道和反映大学生自主创业和到基层就业的内容,并在报道中呈现出其报道的服务性、实用性等特点。     

运用GPS空中校正飞机无线电罗差误差分析

针对某些特种飞机无线电罗差无法沿用传统校正方法在地面进行校正的状况 ,首次提出了运用 GPS接收机在空中校正飞机无线电罗差的方法。本文对影响该校正方法校正精度的各项误差因素进行了分析。     

Security applications of computer vision

In an age which bears witness to a proliferation of Closed Circuit Television (CCTV) cameras for security and surveillance monitoring, the use of image processing and computer vision techniques which were provided as top end bespoke solutions can now be realised using desktop PC processing. Commercial Video Motion Detection (VMD) and Intelligent Scene Monitoring (ISM) systems are becoming increasingly sophisticated, aided, in no small way, by a technology transfer from previously exclusively military research sectors. Image processing is traditionally concerned with pre-processing operations such as Fourier filtering, edge detection and morphological operations. Computer vision extends the image processing paradigm to include understanding of scene content, tracking and object classification. Examples of computer vision applications include Automatic Number Plate Recognition (ANPR), people and vehicle tracking, crowd analysis and model based vision. Often image processing and computer vision techniques are developed with highly specific applications in mind and the goal of a more global understanding computer vision system remains, at least for now, outside the bounds of present technology. This paper will review some of the most recent developments in computer vision and image processing for challenging outdoor perimeter security applications. It also describes the efforts of development teams to integrate some of these advanced ideas into coherent prototype development systems     

SGCMG框架伺服系统动力学建模与低速控制

单框架控制力矩陀螺(SGCMG)框架伺服系统内部存在的各种干扰会严重影响陀螺的力矩输出精度。为了实现力矩输出的高精度控制,需要对框架伺服系统进行精确动力学建模与控制。通过对作用于航天器上SGCMG的详细动力学分析,建立了框架伺服系统动力学模型,其中考虑了动静不平衡干扰力矩以及摩擦力矩。基于正弦永磁同步电机,利用自抗扰理论设计了框架伺服系统内外环控制器。仿真结果表明,在忽略转子不平衡所引起的高频干扰力矩的前提下,此控制器能对内外环存在的所有建模及未建模干扰进行准确估计和补偿,保证了框架的高精度控制。通过仿真还得到了转子不平衡对框架控制精度的影响量级,将为进一步研究如何抑制不平衡振动提供参考依据。     

声强测量的有效性分析及其在国产轻型飞机上的应用

本文对声强测量的有效性作了较全面分析，为精确的声测量奠定了基础。分析结果应用于某型飞机的声强测量中，为该型飞机的降噪工作提供了可靠的数据来源。