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对卫星扩频应答机抗单粒子效应的方法进行分析,设计了采用反熔断丝工艺的FPGA (A54SX32),通过回读比对功能对FPGA 进行监控和处理。此方法大大降低了单粒子效应造成卫星扩频应答机发生功能性故障的可能性,并在系统中通过内部高可靠单机对易发生单粒子效应的扩频应答机进行监控,诊断出故障后进行修复,同时设计定时复位对应答机进行复位、开机操作,确保卫星在轨扩频应答机的正常稳定工作。  相似文献   

4.
针对空间环境辐射效应对低轨(Low Earth Orbit,LEO)卫星固态功放器件的长期影响,以工作超过15年的某卫星发射机为对象,在详细讨论卫星轨道半长轴、倾角、光照角和降交点地方时漂移基础上,分析发射机在轨温度、输出功率等参数变化,重点考察功率长期漂移情况.通过建立模型对功率衰减进行估计,最后结合遥测数据进行检验...  相似文献   

5.
新型星载S波段测控应答机的实现   总被引:6,自引:1,他引:6  
郑伟  金仲和  李灵敏 《宇航学报》2004,25(5):526-530
在改进了传统应答机复杂结构的基础上,设计并实现了适用于皮卫星的体积小、重量轻、功耗低的新型星载S波段测控应答机。该机采用了数字锁相倍频技术和防误锁技术。整个应答机(包括接收和发射部分)在9×9cm2的电路板上实现,功耗小于1w。测试并获得了较好性能,可满足轨道高度小于1000公里的低轨卫星测控要求。  相似文献   

6.
为了提高星座的测试效率、降低测试成本,提出一种适合多星并行测试的应答机设计方法,通过地面测试设备和星上测控应答机复用星上的遥控RS422接口、遥测RS422接口的方式,突破了多星并行测试的瓶颈。新方法已经成功应用于某卫星星座的并行测试,降低了测试成本、提高了测试效率、缩短了星座的测试周期。  相似文献   

7.
Communications transponder for the Japanese Communications Satellite-2 (CS-2a and 2b) to be launched into a geostationary orbit by N-II launch vehicle in February and August, 1983, has been developed. The transponder is provided with six-channel K-band (3020GHz) transponder including beacon transmitter, which operates in the highest frequency ranges ever utilized on an operational communications satellite, and two-channel C-band (64GHz) transponder. Receiver front end of the K-band transponder consists of a direct mixer followed by a 1.8 GHz IF amplifier and provides 8 dB noise figure. 20 GHz output power is 4 W by final amplification at 5-W TWTA. C-band transponder provides 4 dB noise figure and 4.3-W output power. Key factors for future high capacity transponder are also presented.  相似文献   

8.
This paper reports the main characteristics of the deep space transponder (DST) equipment that has been designed, developed and tested by Thales Alenia Space—Italy (TAS-I) for the European Space Agency (ESA) BepiColombo mission to Mercury.  相似文献   

9.
The Centre Français sur les Etats Unis (CFE) held a day-long workshop on GEOSS, GMES and IEOS on 17 January 2006. Sponsored by Arianespace, the invitation-only roundtable drew some 50 participants from European and US administration, industry and academia. The programme and the presentations are on the CFE web site: www.cfe-ifri.net. This report summarizes the proceedings.  相似文献   

10.
偶氮呋咱和氧化偶氮呋咱的合成及表征   总被引:2,自引:0,他引:2  
介绍了高能材料二氨基偶氮呋咱(DAAF)、二氨基氧化偶氮呋咱(DAOAF)及二硝基氧化偶氮呋咱(DNOAF)的合成。其中,采用新型氧化剂制备DAAF,得率提高至65.60%。通过DSC-TG、元素分析、IR、1H NMR和MS等方法,对其结构进行了鉴定,并进行了常规的感度测试。感度数据表明,无氢炸药DNOAF的摩擦感度较大,与C-12相当,而DAAF和DAOAF为低感度炸药。  相似文献   

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受传统观念的影响,人们一般只看到师生人际冲突的负面影响,而很少注意其正面作用;实际上,师生人际冲突是教育教学的互动形式之一,它的存在是必然的,也是合理的,它既有消极有害的一面,也有积极有益的一面。文章试在分析师生人际冲突原因的基础上,针对其影响的二重性,从学校、教师、学生三个方面,提出了正确对待师生人际冲突的建设性对策。  相似文献   

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汽车检测与维护专业是我校重点建设的广西区区级示范专业,经过五年的建设已经形成了一定的规模。文章主要从实验实训中心建设、课程建设、教材建设、师资队伍建设、教学改革等方面对该专业的建设历程进行了回顾和总结。  相似文献   

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On 14 May 2009 the European Space Agency launched 2 space observatories: Herschel (with a 3.5 m mirror it is the largest space telescope ever) will collect long-wavelength infrared radiation and will be the only space observatory to cover the spectral range from far-infrared to sub-millimetre wavelengths, and Planck will look back at the dawn of time, close to the Big Bang, and will examine the Cosmic Microwave Background (CMB) radiation to a sensitivity, angular resolution and frequency range never achieved before. This paper will present the Flight Dynamics, mission analysis challenges and flight results from the first 3 months of these missions.Both satellites were launched on the same Ariane 5 and travelled to the L2 Lagrange point of the sun–earth system 1.5 million km from the earth in the opposite direction of the sun. There they were injected to a quasi-halo orbit (Herschel) with the dimension of typically 750,000 km×450,000 km, and a Lissajous orbit (Planck) of 300,000 km×300,000 km.In order to reach these Lissajous orbits it is mandatory to perform large trajectory correction manoeuvres during the first days of the mission. Herschel had its main manoeuvres on the first day. Planck had to be navigated on the first day and by a mid-course correction manoeuvre, the L2 orbit insertion manoeuvre was planned on day 50. If these slots were missed, fuel penalties would rapidly increase.This posed a heavy load on the operations teams because both spacecrafts have to be thoroughly checked out and put into the correct modes of their attitude control systems during the first hours after launch.The sequence of events will be presented and explained and the orbit determination results as well as the manoeuvre planning will be emphasised.  相似文献   

14.
英汉词语空缺与跨文化差异及翻译策略探究   总被引:1,自引:0,他引:1  
语言是文化的载体,文化上的差异导致了英汉语言中的词汇空缺现象,词汇空缺现象反映了语言的民族性。在跨文化交际中,词汇空缺会给交际带来障碍,造成语用失误,甚至导致交际失败,论文就词语的空缺现象与跨文化差异中的翻译策略进行了一些探讨。  相似文献   

15.
万刚  丛佃伟  刘磊 《宇航学报》2021,42(3):274-283
根据月球测绘的研究现状及发展趋势,对月球测绘学的概念进行了溯源与拓展。在分析月球测绘学与地球测绘学主要差异基础上,从传统测绘学科分类角度出发,综合考虑月球测绘学特殊性,重新梳理出月球测绘学主要学科专业分类,并详细介绍了每个学科专业的定义及国内外研究现状,给出了月球测绘学的五个主要应用领域及其应用展望。我国应尽早开展月球测绘理论与技术研究,形成完整的月球测绘学科体系,能够有力地促进我国空间科学技术的发展,保障后续探月工程的顺利实施。  相似文献   

16.
General Dynamics has now flown all four versions of the Atlas commercial launch vehicle, which cover a payload weight capability to geosynchronous transfer orbit (GTO) in the range of 5000–8000 lb. The key analyses to set design and environmental test parameters for the vehicle modifications and the ground and flight test data that validated them were prepared in paper IAF-91-170 for the first version, Atlas I.

This paper presents similar data for the next two versions, Atlas II and IIA. The Atlas II has propellant tanks lengthened by 12 ft and is boosted by MA-5A rocket engines uprated to 474,000 lb liftoff thrust. GTO payload capability is 6225 lb with the 11-ft fairing. The Atlas IIA is an Atlas II with uprated RL10A-4 engines on the lengthened Centaur II upper stage. The two 20,800 lb thrust, 449 s specific impulse engines with an optional extendible nozzle increase payload capability to GTO to 6635 lb. The paper describes design parameters and validated test results for many other improvements that have generally provided greater capability at less cost, weight and complexity and better reliability. Those described include: moving the MA-5A start system to the ground, replacing the vernier engines with a simple 50 lb thrust on-off hydrazine roll control system, addition of a POGO suppressor, replacement of Centaur jettisonable insulation panels with fixed foam, a new inertial navigation unit (INU) that combines in one package a ring-laser gyro based strapdown guidance system with two MIL-STD-1750A processors, redundant MIL-STD-1553 data bus interfaces, robust Ada-based software and a new Al-Li payload adapter. Payload environment is shown to be essentially unchanged from previous Atlas vehicles. Validation of load, stability, control and pressurization requirements for the larger vehicle is discussed.

All flights to date (five Atlas II, one Atlas IIA) have been successful in launching satellites for EUTELSAT, the U.S. Air Force and INTELSAT. Significant design parameters validated by these flights are presented. Particularly noteworthy has been the performance of the INU, which has provided average GTO insertion errors of only 10 miles apogee, 0.2 miles perigee and 0.004 degrees inclination. It is concluded that Atlas II/IIA have successfully demonstrated probably the largest number of current state-of-the-art components of any expendable launch vehicle flying today.  相似文献   


17.
国际上发射的海表盐度遥感卫星主要有2颗:欧洲的SMOS和美国的Aquarius卫星,为给后续海表盐度遥感提供参考借鉴,对比分析了这2颗卫星的遥感器载荷、数据处理算法和盐度数据。遥感器载荷方面,SMOS采用L波段二维综合孔径辐射计,而Aquarius采用L波段实孔径辐射计加散射计;数据处理算法方面,分析了二者在介电常数模型、海面粗糙度校正以及反演算法方面的差异;盐度数据方面,分析了SMOS与Aquarius盐度数据之间的相关程度,并分别与ISAS(In Situ Analysis System)浮标盐度数据作对比,分析了2颗卫星的盐度数据精度。将2颗卫星的盐度遥感数据与ISAS浮标盐度数据对比发现,在全球范围内,Aquarius盐度测量精度优于SMOS;但在开阔海域,SMOS盐度测量精度优于Aquarius;而在近海岸区域,均出现较大的误差,且SMOS数据误差更大。  相似文献   

18.
凝胶推进剂及其模拟剂的制备和特性表征   总被引:1,自引:0,他引:1  
代玉东 《火箭推进》2004,30(2):59-64
高能凝胶推进剂的选择、制备、实验及特性表征是凝胶推进剂研究的关键环节.燃料凝胶化包括有机和无机两种胶凝剂.氧化剂的凝胶化使用了无机胶凝剂.此外选择和配制了凝胶推进剂的模拟剂,它具有与实际燃料和氧化剂相匹配的流变特性.制备了在流变学上相匹配的凝胶燃料和凝胶氧化剂、惰性凝胶模拟剂与凝胶推进剂,并对其流变学特性进行了分类.  相似文献   

19.
Rigorous bed rest (RBR) induces significant biochemical and circulatory changes. However, little is known about acute rigorous bed rest (ARBR). Measuring biochemical and circulatory variables during ARBR and RBR the aim of this study was to establish the significance of ARBR effect. Studies were done during 3 days of a pre-bed rest (BR) period and during 7 days of ARBR and RBR period. Thirty normal male individuals aged, 24.1 +/- 6.3 years were chosen as subjects. They were divided equally into three groups: 10 subjects placed under active control conditions served as unrestricted ambulatory control subjects (UACS), 10 subjects submitted to an acute rigorous bed rest served as acute rigorous bed rested subjects (ARBRS) and 10 subjects submitted to a rigorous bed rest served as rigorous bed rested subjects (RBRS). The UACS were maintained under an average running distance of 9.7 km day-1. For the ARBR effect simulation, ARBRS were submitted abruptly to BR for 7 days. They did not have any prior knowledge of the exact date and time when they would be asked to confine to RBR. For the RBR effect simulation, RBRS were subjected to BR for 7 days on a predetermined date and time known to them right away from the start of the study. Plasma renin activity (PRA), plasma cortisol (PC), plasma aldosterone (PA), plasma and urinary sodium (Na) and potassium (K) levels, heart rate (HR), cardiac output (CO), and arterial blood pressure (ABP) increased significantly, and urinary aldosterone (UA), stroke volume (SV) and plasma volume (PV) decreased significantly (p<0.05) in ARBRS and RBRS as compared with their pre-BR values and the values in UACS. Electrolyte, hormonal and hemodynamic responses were significantly (p<0.05) greater and occurred significantly faster (p<0.05) during ARBR than RBR. Parameters change insignificantly (p>0.05) in UACS compared with pre-BR control values. It was concluded that, the more abruptly muscular activity is restricted in experimental subjects while they are very active, the greater hemodynamic and biochemical change there is and probably in individuals whose muscular activity is abruptly terminated after an accident or sudden illness.  相似文献   

20.
于佳  宗鹏 《宇航学报》2011,32(1):172-178
需要一个平台对探月卫星,探月图像传输和处理进行研究. 嫦娥一号月球图像的传输与处理的仿真,结合了链路分析,采用MATLAB GUI 和虚拟现实设计工具。由于图像在深空传输中,距离较远,信号会受到很大的衰减,传输质量会受到噪声干扰的严重影响。因此要对系统链路进行严格的预算分析,包括考虑地球大气产生的影响,以确保信号传输质量满足要求,另外还要通过适当算法提高图像的清晰度。这种仿真方法对探月图像传输的研究奠定了基础,并且对降低探月成本有一定的帮助。  相似文献   

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