虚拟仪器测试技术应用综述

介绍了虚拟仪器测试技术的基本概念、虚拟仪器结构和虚拟仪器总线技术，讨论了面向对象的虚拟仪器测试系统的开发与虚拟仪器测试系统软件设计。     

虚拟仪器技术的测试系统设计与标准化运用

从虚拟仪器的定义、硬件和软件的构成、虚拟仪器技术在测试系统设计中的应用等几方面进行了较详细的探讨;指出系统接口和软件接口的标准化、通用化是虚拟仪器技术应用的关键;对虚拟仪器技术在工程上运用时应注意的几个有关标准化问题提出了自己的看法.     

基于虚拟仪器技术的TACAN 综合测试仪的开发

简要介绍了虚拟仪器的概念、结构,然后着重介绍用于机载TACAN综合测试的虚拟仪器系统的设计与开发.给出硬件构成原理,采用LabWindows/CVI作为虚拟仪器软件的开发平台.     

虚拟仪器测试技术综述

介绍了虚拟仪器基本概念及其软硬件结构，讨论了虚拟仪器总线系统，总结了虚拟仪器测试系统的特点。     

一个虚拟仪器的系统结构分析与设计

分析了一个虚拟仪器的硬件系统和软件系统,并描述了该虚拟仪器的设计实现,探讨了虚拟仪器在军事中的应用.     

虚拟仪器及其发展前景

通过概括介绍虚拟仪器的概念、组成、特点及分类，阐述了虚拟仪器未来的发展方向和应用前景，尤其是在电子技术实验教学中的应用广泛。     

虚拟仪器计量评价中的几个问题

本文讨论了虚拟仪器计量评价所面临的几个特殊问题，提出了将虚拟仪器性能分为仪器基本硬件平台的性能以及软件和数学模型的性能两个方面的设想，最后给出了虚拟仪器计量解决方案     

虚拟仪器及其对军用ATE发展的影响

自动测试设备（ＡＴＥ）在现代飞行器及先进的武器装备及其电子设备的设计，生产和维护／维修过程中都起着关键的作用。本文介绍了虚拟仪器的概念、硬件平台和软件结构、主要特点以及虚拟仪器软件开发工具，概述军用ＡＴＥ的发展状况，讨论虚拟仪器对军用ＡＴＥ发展的影响。虚拟仪器（Virtual Instrument VI）概念 是ＮＩ公司于１９８６年首先提出的，其基本思想是在一定的硬件环境（或平台）支持下，通过编制和执行不同的虚拟仪器软件，来构成各种不同的仪器，实现各种用户定义的仪器或测试功能。传统仪器中，仪器功能是用仪器箱内的硬件…     

基于LabVIEW的虚拟电工实验室的研制

主要介绍了虚拟仪器技术在电工实验室中的应用,并借助LabVIEW编程平台设计了电工实验室中4个最为常用的虚拟仪器设备示波器、频谱分析仪、信号发生器和数字电压表.     

LabVIEW在信号分析虚拟仪器中的应用

采用虚拟仪器技术,重点介绍了两种关于信号分析的虚拟仪器:联合时频分析和小波分析虚拟仪器,应用于航空发动机转子实验室的信号测试与分析系统。为振动信号的分析和航空发动机故障诊断中提供分析手段。     

UVCS/SOHO Observations of Spectral Line Profiles in Polar Coronal Holes

Ultraviolet emission line profiles have been measured on 15-29 September 1997 for H I 1216 Å, O VI 1032, 1037 Å and Mg X 625 Å in a polar coronal hole, at heliographic heights ? (in solar radii) between 1.34 and 2.0. Observations of H I 1216 Å and the O VI doublet from January 1997 for ? = 1.5 to 3.0 are provided for comparison. Mg X 625 Å is observed to have a narrow component at ? = 1.34 which accounts for only a small fraction of the observed spectral radiance, and a broad component that exists at all observed heights. The widths of O VI broad components are only slightly larger than those for H I at ? = 1.34, but are significantly larger at ? = 1.5 and much larger for ? > 1.75. In contrast, the Mg X values are less than those of H I up to 1.75 and then increase rapidly up to at least ? = 2.0, but never reach the values of O VI.     

A Digital System for Accurate Time Sector Division of a Spin-Stabilized Vehicle

This paper describes an aspect system flown on PIONEERS VI and VII2 which incorporates an extremely accurate adaptive digital computer in order to define rigorously equal time intervals which are submultiples of the spacecraft spin period. The several submultiples which compose the complete spin period exhibit equality to within 2.5 parts in 105. This system has potential applications in other experiments involving the study of the angular dependence of cosmic radiation and other physical phenomena being measured by a single directional detector mounted on spin-stabilized spacecraft. Included here are the scientific goals for this experiment, system restraints, and the generalized system operation. Some details on specific logic and hardware implementation for the Pioneer experiments are included along with in-flight performance evaluation of the system aboard PIONEER VI.     

Developing a visual component library for a graphical programmingplatform using object orientation

The development of virtual instruments (VIs) is bringing a great revolution to the fields of automated testing and measurement. It is accelerating the integration of measurement systems and is promoting instrument standardization, modularization and generalization. A graphical programming platform for automated testing is one of the most important applications of VI technology, and it provides users with an intuitive and friendly programming environment. The visual component library (VCL) is the key part of such graphical programming platforms. The research reported in this paper makes full use of the advantages of the object-oriented methodology to develop the visual VI components for a graphical programming platform. By setting up two base classes for all the VI components, various VIs can be efficiently developed     

基于虚拟仪器的轮翼气动实验系统研究

针对一种用于小型飞行器的新型高效升力和推力系统——轮翼,为了解决其所面临的测量参数多、气动力/力矩量值小、实时性强、耦合性高的困难,研制了基于虚拟仪器（VI）的气动实验系统。该系统采用四分量高精度应变天平、AC伺服电机及驱动器、应变放大器等设备搭建实验平台,利用基于虚拟仪器的LabWindows/CVI软件进行数据采集和数据处理。实验测得天平输出信号电压值与软件采集记录结果一致,为进一步做模型试验提供了可靠的基础。     

Comparison of Polar and Equatorial Coronal Holes Observed by UVCS/SOHO: Geometry and Physical Properties

We analyzed UVCS/SOHO data and compared the H I Lyα (121.6 nm) and O VI (103.2 nm, 103.7 nm) emission in the polar and equatorial coronal holes. We found that the emission lines have similar characteristics in these two types of coronal holes. Both types show evidence for superradially diverging boundaries. The latitudinal distribution of the O VI line ratio may indicate that the equatorial coronal hole has O⁺⁵ outflow velocities lower than in the polar coronal holes. This revised version was published online in June 2006 with corrections to the Cover Date.     

On the Lyman α and O VI Line Profiles in Streamers and Coronal Holes

The profiles of the Lyα line at 1215.6 Å and of the O VI doublet at 1031.9 Å and 1037.6 Å in the extended solar corona have been analyzed vs. latitude and radial direction, performing observations with the Ultraviolet Coronagraph Spectrometer (UVCS) on board the ESA-NASA solar satellite SOHO (Solar and Heliospheric Observatory). The results show that these lines behave differently with latitude: the H I Ly α line has larger full width at half maximum (FWHM) values in the streamer region and narrower values towards the pole, while the FWHM of O VI lines has a minimum at the center of the streamer and slightly increases towards the polar regions. We briefly discuss the impact of the results on coronal heating theories.     

Local Interstellar Medium Summary of Working Group VI

This report summarizes the issues discussed in Working Group VI concerning the accuracy of measurements of D/H and 3He/H in the local interstellar medium, possible systematic errors, and emerging trends in the results.     

嵌入式Internet技术及其在基于Web的虚拟仪器中的应用研究

描述了嵌入式Internet系统的一种实现和基于Web的虚拟仪器的概念，介绍如何利用嵌入式Internet技术构造基于web的虚拟仪器（VI）。     

Compact equipment for on-board communications subsystem supervisoryand control system

Onboard equipment for the communications subsystem supervisory and control (CSC) system of a next-generation multibeam high-capacity communications satellite is discussed. In order to keep the equipment as compact, lightweight, and low in power consumption as possible, an onboard data bus system using four kinds of LSIs was developed. It will be carried on-board the Japanese Engineering Test Satellite VI for launch in 1993. Configuration and functions of the CSC equipment, design philosophy of the LSIs, and characteristics of the LSIs developed are discussed     

航电系统外场保障实习台的设计与研究

根据航电系统在外场通电时对操作人员的技能要求和相关设备需求,提出了研制航电系统外场保障实习台的思路和方案;构建了实习台的半实物仿真模型,设计了基于模拟操作功能的硬件电路,编制了基于虚拟仪器技术的软件流程,完成了实习台的系统集成与调试,实现了航电系统外场通电保障的模拟训练;应用结果表明,实习台功能强,可扩展性好,使用广泛,军事经济效益显著。