Study of satellite situations mission

Problems of situational investigations during the planning and control of the space experiment in the near-Earth space are considered in this paper. It gives the concept of the orbital torus and shows its application in various problems of situational investigations: the forecast of intersections of the orbit with the magnetopause and bow shock, regions of satellites radiovisibility from the ground observation post and others.     

浅析新形势下党务工作

2008年全球金融危机爆发,世界经济遭遇前所未有的重创,做为与国民经济息息相关的中国民航运输业,虽然我国经济形势相对较为稳健,但也受到了一定的冲击。2008年青海空管分局党委在上级党委的领导下,以“三个代表”重要思想和十七大精神为指导,认真贯彻落实科学发展观,围绕“安全、和谐、进步”的主题,把安全生产作为党委工作的中心任务,充分发挥党委的政治核心作用,党支部的战斗堡垒作用,党员的先锋模范作用和干部的表率作用,全面加强党建政治思想工作和党风廉政建设,     

红外头罩电弧风洞试验状态的量化新判据

提出了一种红外空空弹红外头罩电弧风洞试验状态的量化新判据.研究表明:热应力是导弹高速飞行时头罩应力的最大影响因素,可用最大热应力作为电弧风洞试验状态的确定判据取代目前国内现有试验状态确定判据.通过准确的气动热应力计算,可保证红外头罩的电孤风洞试验状态与飞行环境的一致.     

民用航空电信人员现状分析

通信导航监视设施设备是民航空管系统的重要组成部分,民用航空电信人员作为从事民用航空通信导航监视设备保障工作的技术人员,在空管设备运行保障工作中承担着重要的作用。目前民用航空电信人员按照执照专业分为地空通信、平面通信、导航、雷达、自动化处理系统、飞行校验和附属设备七类,各专业根据不同设备类型细分为不同的岗位类别。随着空管业务和新技术的不断发展、应用,     

如何做好新形势下民航新闻宣传工作

新闻宣传工作是我们党的政治优势,是党的思想政治工作的重要组成部分,是文化建设的有力抓手和重要载体。胡锦涛总书记强调指出,做好新闻宣传工作,关系党和国家工作全局,关系改革和经济社会发展大局,关系国家长治久安。做好民航的新闻宣传工作,是树立行业形象、鼓舞员工士气、增强单位凝聚力、确保安全生产的有力手段。当前,我国经济社会发     

Safety implications of unscheduled situations in the operation of tethered satellite systems from the international space station

Space based experiments involving the use of tethers were examined with a view to identifying the implications of unscheduled events such as tether severance and interference between the tether and other hardware. It is the authors opinion that these type of events, which have important consequences for the operation of tethers in space, have received insufficient consideration in the extensive literature on the subject. In particular, the investigation of the interference event appears to be completely new. The examination focussed on tether experiments planned for the forthcoming International Space Station (ISS). Results were obtained through the use of a highspeed, non-linear, computer simulation model specifically designed for use with tethered satellite systems. Simulations showed that both severance and interference were possible during retrieval of the tether, particularly if ‘skip-rope’ motion is initiated. The motion following each of these incidents is predicted and shows that these unscheduled events are potentially very hazardous for the ISS. While the results of these simulations are not directly applicable to specific operations on the ISS, they fulfill the primary purpose of this paper which is the demonstration of this new technology.     

北京终端管制区扇区现状分析及未来规划展望

引言近年来,民航业的迅猛发展以及旅客吞吐量和飞行运行总架次的日益增长,使得我国空中交通系统面临着越来越严峻的挑战,多个国际枢纽及区域枢纽机场出现严重的拥挤,空中交通管制员在其管辖空     

一次冻雨天气过程与典型冻雨形势差异分析

引言冻雨也叫雨凇,是过冷却雨滴与地面或地物、飞机等相碰而即刻冻结的雨。冻雨天气是冬半年降水中的一种特殊情况,冻雨天气虽然出现不多,但对民航的危害较大。     

FY-2G Launched Successfully

<正>The FY-2G meteorological satellite was launched into space by a LM-3A launch vehicle at 09:02(Beijing time)on December 31,2014 from the Xichang Satellite Launch Center.24 minutes after the liftoff,the satellite separated from the rocket and entered its preset orbit.The satellite was positioned in a geosynchronous orbit above the     

以科学发展观为统领 着力抓好新形势下基层员工的思想工作

温家宝总理在省部级主要领导干部专题研讨班作报告时强调：要把各方面的积极性引导到科学发展上来,实现更长时间、更高水平、更好质量的发展。     

刀具半径补偿功能在数控加工中的一种应用

介绍了在数控机床中使用刀具半径补偿功能(G41、G42)，实现利用同一段数控程序完成对余量较大的工件进行多次走刀加工的方法。     

刀具半径补偿功能在数控加工中的一种应用

介绍了在数控机床中使用刀具半径补偿功能(G41、G42),实现利用同一段数控程序完成对余量较大的工件进行多次走刀加工的方法.     

第三代移动通信系统中非线性多用户检测技术

在CDMA系统中，多用户检测技术是提高系统容量，减少用户间干扰的关键。非线性多用户检测包括干扰消除和神经网络检测技术。其中干扰消除检测是对不同用户独立进行MAI估计，然后从接收信号中减去对该用户而言的部分或全部MAI；多用户检测从本质上看是一个组合优化问题，所有解决组合优化的算法原则上均可适用于多用户检测，其中基于神经网络的解组合优化方法当然也适用于多用户检测。本文论述了几种非线性多用户检测器的基本原理及其特点。     

第三代移动通信系统中非线性多用户检测技术

在CDMA系统中,多用户检测技术是提高系统容量,减少用户间干扰的关键.非线性多用户检测包括干扰消除和神经网络检测技术.其中干扰消除检测是对不同用户独立进行MAI估计,然后从接收信号中减去对该用户而言的部分或全部MAI;多用户检测从本质上看是一个组合优化问题,所有解决组合优化的算法原则上均可适用于多用户检测,其中基于神经网络的解组合优化方法当然也适用于多用户检测.本文论述了几种非线性多用户检测器的基本原理及其特点.     

Degraded EEG response of the human brain in function of gravity levels by the method of chaotic attractor

The measurement of the influence of different gravity levels on the brain allows to explain how humans react to microgravity in space and to predict the adaptation capability of astronauts. Human electroencephalographic (EEG) signals were recorded during low and high gravity phases of three consecutive days of parabolic flights on the Caravelle aircraft in 1991. EEG signals were processed, using the method of correlation dimensions d of chaotic strange attractors. Results show clear differences between the three flights, with a general decrease over time in the attractor dimensions, a measure of the brain response to changing g levels. However, the dimension is not a one-to-one relation with g levels, as additional variations are observed. Two hypotheses are introduced, the "fatigue/stress" and the "g stress" hypotheses corresponding, respectively, to long-term fatigue accumulated over the three flights, and to short-term fatigue in response to change in g levels. The former explains the overall decrease of dimensions, the latter yields additional variations on shorter time scales. As the brain response degrades with time, at least six degraded modes were observed, explained by both short- and long-term fatigue.     

IPv6在3G卫星通信系统中的发展模式探讨

面对地面3G演进和NGN（Next Generation Network）的发展趋势,以空间段为基础的3G卫星通信系统与技术应该扮演怎样的重要角色、如何进一步发展,已成为一个紧迫的研究课题。文章在分析NGN对于卫星通信发展影响的基础上,介绍了目前IPv6技术的空间应用以及3G业务在卫星中的应用模式,并对IPv6技术在3G卫星通信系统中的发展模式进行了探讨。     

CBERS地面接收系统G/T值测量

利用宇宙射电源测量地面接收系统品质因数Ｇ／Ｔ值是大多数地球站普遍采用的测量方法。本文针对中国科学院遥感卫星地面站ＣＢＥＲＳ接收系统给出系统Ｇ／Ｔ值测量需要的射电源流量密度和修正系数计算公式以及测量误差分析。最后，根据ＣＢＥＲＳ系统工厂验收测试遇到的问题，对不同天线仰角间的Ｇ／Ｔ值换算进行分析。分析表明：不同天线仰角间的Ｇ／Ｔ值可以换算，ΔＧ／Ｔ等于不同天线仰角下测量的背景冷空噪声功率之差。     

FY-2G Joins FY Meteorological Satellite Family

<正>At 09:02 Beijing time on December31,2014,a LM-3A launch vehicle successfully launched the FY-2-08meteorological satellite from the Xichang Satellite Launch Center.The satellite was positioned at 99.5°E over the equator in geostationary orbit at 07:40 on January6,2015.The satellite was designated as FY-2G after it entered its orbit successfully.