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介绍美国开放式遥测地面站、微机遥测地面站的特点及其发展动向。主要的发展包括大力推行宇航CCSDS标准;遥测标准部分内容改变、开放式遥测地面站、完成(或正在完成)IRIG、CCSDS标准兼容扩展。结论认为:对于运载工具、卫星、载人航天器的航区,宜用开放式遥测站。而实验室、较小的弹及要求不太高的飞行器射前检测,宜用微机遥测站。 相似文献
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新型的双环锁相极化分集接收机 总被引:1,自引:0,他引:1
介绍了七○四所研制成功的我国新一代靶场遥测换代产品-TMR极化分集接收机。该机具有极化分集、微机控制遥测、实时变程序遥测、角误差解调等多种功能。文中介绍了该机的主要技术指标、工作原理、主要技术关键。重点分析了新型的双环销相极化分集技术及其实现方法。本机已成功地应用于航天靶场、海军靶场的YQ311工程、8710工程遥测系统及铱星地面检测站等多种型号任务中. 相似文献
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PCM遥测信号源的设计与实现 总被引:2,自引:0,他引:2
给出一种基于 EPROM的遥测模拟信号源的设计方案及其实现方法。通过计数器传送地址信号 ,读取烧制在 EPROM里的动态信号码并与计数器本身产生的固定码相结合 ,从而形成多路串行的遥测模拟信号源。该信号源可用于产生各种格式的遥测帧结构 ;可用它对地面视频设备进行调试和性能检测 ;可作遥测专业实践教学的模拟信号源 ,以便了解遥测帧结构。因此 ,它可作为地面遥测站的模拟信号源 ,也可作为其它实验板的输入信号源。格式多样 ,使用方便。 相似文献
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一、同步的作用及其方式在数字遥测系统中,同步是一个十分重要的问题。一个遥测系统能否正常工作,在很大程度上取决于同步的质量。若同步不良,将导致遥测质量下降,甚至使遥测失效。我们知道,数字遥测所传送的是数字信号。这些信号是从发端一位一位地发送的,然后在收端一位一位地接收。为了将收到的信号复原,就要对码元进行正确无误的判决。这就要求判决用的 相似文献
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介绍基于10Mbps弹(箭、星等)载分布式遥测系统结构及其中心控制器的设计。基于串行总线的分布式遥测系统具有电缆网少、组成灵活、就近采集参数等优点,适于大型飞行器的测量要求。随看我国航空航天技术的发展,分布式拓扑结构的遥测系统已逐渐显示出它的优势。我们已经把分布式遥测系统作为弹上设备的基本型进行研制,并已完成原理性实验和联试,系统最高码速率可达到5Mbps。 相似文献
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为使某武器在定型阶段能测量一些特殊参数,研制了频分制(FM-FM)遥测地面站。介绍了该地面站的主要技术指标、功能及设计时必须考虑的几个总体问题。靶试表明,该地面站的设计是正确的。 相似文献
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“国际空间站”系统特点分析 总被引:1,自引:1,他引:0
介绍了"国际空间站"的总体设计;分析了"国际空间站"系统设计的特点和不足,其中包括重视成熟技术和冗余设计,众多系统故障暴露出技术薄弱性,机器人系统自动化水平有待提高,以及许多先进技术规划未能实施;提出了发展中国空间站的启示与建议,如借鉴国外协力合作系统先进设计经验和科学评估安全性方法,权衡技术继承性与先进性,注重空间站系统设备的设计、维修、机器人开发和延寿问题。 相似文献
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A. V. Rodnikov 《Cosmic Research》2006,44(1):58-68
The motion of a space object in the gravitational field of the Earth is considered. The object consists of an extended space station and a weight, which is free to move along the cable fixed to the ends of the station. It is assumed that the station is composed of two masses coupled by a weightless rod, while the cable is weightless and non-stretched. The equations of motion of such a system are derived for the case when the motion proceeds in a single plane, while the center of mass of the system moves along a circular geocentric orbit. The conditions of the cable tension (conditions of being on tie) are derived. The phase portrait of the weight motion along the cable is constructed when the station is oriented to the attracting center or is perpendicular to this position. The possibility to leave the tie in this case is analyzed. Equilibrium configurations of the system are found, i.e., such motions of the object under consideration at which the weight does not change its position relative to the station. Lyapunov stability of such configurations is analyzed for two situations: when the station is composed of equal masses and when masses at the ends of the station are different. In particular, for the case of different masses it is established that there exist such positions of equilibrium at which the dumbbell is located at an angle to the direction to the attracting center. In some cases these positions can be stabilized (if the weight is fixed on the cable). 相似文献
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V. V. Sazonov M. Yu. Belyaev N. I. Efimov V. M. Stazhkov E. V. Babkin 《Cosmic Research》2001,39(2):126-136
We describe the determination of the quasistatic component of microaccelerations, as it was done during the space experiments with the instruments DACON and ALICE-2. This component was calculated using the telemetric information related to the motion of the station with respect to its center of mass. The information consists of the values of the station angular velocity vector and the quaternion which specifies its orientation, determined at discrete instants of time. The quaternion is determined with a step of about 1 min, the angular velocity with a step of about 10 s. The information is used in the following manner. At first, the quaternion components corresponding to some time interval are smoothed by splines. Then, employing the obtained splines and kinematic equations, the angular velocity and acceleration of the station are calculated on this interval. Finally, the microacceleration is calculated as a function of time at the point of the location of the instrument. The data of measurements of the angular velocity are used for the purpose of control. As a rule, the available telemetric information allows one to find the quasi-static component for the entire time interval of carrying out the experiment. Examples of determination of this component for some experiments are presented. A comparison with the results of calculating the microacceleration quasistatic component by other methods is made. 相似文献
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空间站能源系统并网供电技术研究 总被引:1,自引:0,他引:1
空间站结构复杂,通常由多个舱段组成,与飞船等飞行器进行交会对接后,各舱段和对接飞行器自有的能源系统可能会由于空间位置及相互遮挡等原因而无法满足自身供电需求,这就需要对舱体电源系统进行并网供电。文章论述了“天宫一号”目标飞行器与“神舟”飞船采用的并网供电方案,通过并联冗余及自动均流控制实现不同舱体间的功率传输;在此基础上,通过调研国外空间站并网供电技术,比较了空间飞行器组合体并网供电中的技术方案及特点,总结了目前空间站并网供电模式可采用的类型,最后提出了我国未来空间站并网供电可采取的方案。 相似文献
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针对采用100V高压电池阵的空间站结构体带电现象,提出采用等离子体接触器进行主动电位控制方案,根据此方案建立包含接触器的空间站充放电等效电路模型,研究等离子体接触器对空间站充放电过程的影响及空间站结构因素对接触器钳位效果的影响,从而了解等离子体接触器与空间站悬浮电位的耦合特性。结果表明,无论空间站处于“快速充电”还是“正常充电”情况,等离子体接触器均能有效将空间站悬浮电位钳制在合理范围内。空间站结构因素中,电池阵暴露导体面积对接触器钳位过程影响较大,结构体暴露导体面积和结构体等效电容的影响可忽略。 相似文献