共查询到19条相似文献，搜索用时 109 毫秒
1.
《天文研究与技术》2016,(2)
以极地天文望远镜为应用背景,研制了一种低温微位移促动器,并在室温和低温条件下进行性能测试实验,获得了低温微位移促动器的性能指标。分析了3种常见的大行程高精度微位移促动器的结构形式,选择位移缩放式作为低温微位移促动器的基本结构。微位移促动器采用低温步进电机作为驱动元件,以具有特殊消隙结构的螺旋传动作为位移缩放机构,实现了高刚度、耐低温、结构紧凑、密闭性好的微位移促动器的设计。开展了微位移促动器的性能测试实验,结果表明:所设计的低温微位移促动器在室温条件下的步进精度达到1μm±0.082μm,并且满足负载能力的设计要求;低温条件下步进精度可以达到2μm±0.404μm。研制的微位移促动器将为拼接式极地天文望远镜的建设提供重要的技术支持。 相似文献
2.
随着光学天文望远镜口径不断增大,望远镜主镜多采用拼接镜面形式,而微位移促动器作为镜面拼接技术的关键部件,始终是研究的热点之一。以双螺旋滚珠丝杆代替传统机械式微位移促动器中减速器加滚珠丝杆结构,利用差动螺旋原理进行微位移输出,使用伺服电机作为驱动电机,并对负载时电机所需的转矩进行分析。微位移促动器的输出位移精度、行程及负载能力是重要技术指标,本文从这三方面的要求出发,开展性能测试。实验结果表明,该微位移促动器总行程为5 mm,理论最大可承载1 200 N,在200 N的负载下实现200 nm的步长分辨率,开环单向位移精度优于0.65μm,闭环单向位移精度优于0.2μm。验证了所提出的微位移促动器具备高精度、大行程和高负载的要求,为我国未来大口径天文望远镜的设计提供技术储备。 相似文献
3.
以环形太阳望远镜为应用背景,研制了一种基于步进电机的位移促动器,并进行了性能测试实验,获得了位移促动器的性能指标。分析了常见的大行程、高精度位移促动器的结构形式,选择位移缩放式作为位移促动器的基本结构。该位移促动器采用步进电机集成行星减速器作为驱动元件,以具有特殊消间隙结构的螺旋传动作为位移缩放机构,为实现高分辨率、高刚度和高精度的位移促动器设计,开展了位移促动器的性能测试实验,结果表明:该位移促动器轴向位移量程为±2 mm,不同负载下均能实现1 μm的步长分辨率,位移闭环输出精度优于1 μm。研制的位移促动器为环形太阳望远镜的建设提供重要的技术支持,并为其它精密光学镜面支撑系统的工程应用提供参考。 相似文献
4.
5.
介绍拼接镜面主动光学计算机控制的设计思想和研制的方法。计算机通过接口控制6套微位移促动器实现了同步工作;控制维持三块子镜的共焦和共面;采用6套电容式的微位置传感器来检测共面的位置,作为计算机闭环控制的反馈信号。位移促动器的控制分辨率为5nm左右。系统控制的位置误差rms值小于25nm。 相似文献
6.
针对2 m环形太阳望远镜主镜轴向支撑设计需求和指标,研制了一种基于波纹管的气压式力促动器,开展了全面实验测试。该气压式力促动器采用可伸缩高强度、高弹性金属波纹管作为核心器件,采用线性轴承作为导向机构,并集成单向压力传感器作为力反馈元件,同时在设计中考虑了安装调整工艺便捷性。经测试,该气压式力促动器单向输出力达200 N,输入气压与输出力线性度误差小于2%,力分辨率小于0.23 N,闭环力精度优于±0.3 N。测试结果验证了该气压式力促动器原理和结构简单,安装维护工艺良好,达到了设计指标,可满足2 m环形太阳望远镜主镜轴向支撑的需求。研制工作为气压式力促动器的设计细节改进及主镜支撑系统的工艺优化奠定了基础,并可为其它精密光学镜面支撑系统的工程应用提供参考。 相似文献
7.
8.
随着毫米波天文学和空间通信的重要性日益提高, 对天线性能提出了越来越高的要求, 而天线性能往往受到其反射器表面精度的限制. 微波全息技术是一种快速有效的检测反射面天线表面轮廓的测量技术. 通过微波全息测量得到天线口径场, 计算天马65m射电望远镜反射面与理想抛物面的偏差. 天马65m射电望远镜的主反射面板是放射状的, 有14圈. 面板的每个角都固定在面板下方促动器的螺栓上进行上下移动, 且相邻面板交点处的拐角共用一个促动器. 采用平面拟合的方法可以计算各块面板拐角处的调整值, 但是同一个促动器会得到4个不同的调整量. 通过平面拟合, 同时以天线照明函数为权重的平差计算方法得到相邻面板拐角的一个平差值, 即天马65m射电望远镜1104个促动器的最佳调整值. 通过多次调整和新算法的应用, 天马65m射电望远镜反射面的面形精度逐渐提高到了0.24mm. 相似文献
9.
为满足大口径地面射电望远镜的高精度要求,开展射电望远镜热影响研究,保持结构的热稳定性,对提高望远镜指向精度有重要意义。以改造后南山26 m天线为研究对象,利用FEMAP软件建立座架结构模型,设定边界条件,得到某年6月4日全天各时刻天线座架上的温度场分布,将温度场结果与结构耦合,得到热变形,建立了温度测量系统,与仿真结果相比,当天局部最高温度可达31.33℃,最大温差可达10℃,最大位移量可达1.8 mm,与实测结果变化规律基本一致。分析座架温度分布规律及其变形影响,为后期天线的温度补偿和结构优化提供参考依据。 相似文献
10.
11.
An Improved Grey Model and Its Application Research on the Prediction of Real-time GPS Satellite Clock Errors 总被引：2，自引：0，他引：2
In the work on the real-time GPS precise point positioning, the realtime and reliable prediction of the satellite clock error is one of the keys to the realization of the GPS real-time high accuracy point positioning. The satelliteborne GPS atomic clock has high frequency, is very sensitive and extremely easy to be influenced by the outside world and its own factors. Therefore, it is very difficult for one to know well its complicated and detailed law of change, with these attributes being in accordance with the characteristics of the theory of grey system. Thus, it is considered that the process of variation of the clock error is regarded as a grey system. On the basis of the exploration of the limitations of the quadratic polynomial and grey model satellite clock error predictions, the research on the real-time prediction of the GPS satellite clock error by taking advantage of the improved grey model is proposed. Finally, the materials of the GPS satellite clock error of 3 different time intervals are used to make the accuracy analysis of the clock error prediction of different sampling intervals, to study the relation between the grey model exponential coefficient and the prediction accuracy and to make the analysis of the comparison of the prediction accuracy with that of the quadratic polynomial method. The general relation between the different types of satellite clock errors and the model exponential coefficients is summarized and compared with the IGS final clock error ephemeris product to test and verify the feasibility and availability of the improved prediction model proposed in the present article so as to provide the higher-accuracy satellite clock error products for the real-time GPS dynamic precise point positioning. 相似文献
12.
《Chinese Astronomy and Astrophysics》2023,47(2):391-409
Position prediction is the basis of guiding radar to seek, capture, and track space targets, although there’s a risk of insufficient accuracy for narrow beam radar due to the influence of orbit determination and propagation error. Since the along-track error is the main factor that affects the accuracy of position prediction, this paper proposed a Constant Elevation Search (CES) method for narrow beam radar, based on the idea of along-track error compensation, to seek and capture transit targets. With along-track error estimation, all possible positions on a specified elevation can be observed, thus the success rate of capturing transit targets will be improved. Simulation shows that when the position prediction method fails, the CES method still works. 相似文献
13.
14.
区域北斗星基增强系统提供等效钟差改正数统一修正星历和钟差误差。随着系统的建设发展,新一代北斗星基增强系统将区分星历和钟差误差改正信息,以提高差分改正精度。由于北斗卫星混合星座设计及区域监测网的局限,星历和钟差误差的高精度分离计算面临着新的挑战。对北斗星基增强系统的星历和钟差改正算法进行了研究,分别采用动力学和运动学模式计算了卫星星历和钟差改正数,并基于北斗实测数据,对两种处理模式的差分改正精度进行了对比研究。试验结果表明,采用动力学和运动学差分方法,得到的双频伪距实时定位精度分别为1.76m和1.78m,定位精度与WAAS及EGNOS相当。利用运动学和动力学差分改正数后均可得到分米级的精密单点定位(precise point position,PPP)结果,其中采用动力学广域差分改正数,收敛后定位精度可达到15cm;采用运动学广域差分改正数,收敛后定位精度可达45cm。 相似文献
15.
为了研究低轨通信卫星多普勒定位性能,首先分析了低轨卫星的对地覆盖特性、信号传输特性以及多普勒频移特性,推导了多普勒定位原理和方法,提出了适用于多普勒定位的精度因子.基于已在轨的铱星和全球星系统,解算了全球范围可见卫星数和定位精度因子,并对相应测站进行了定位仿真实验和误差分析.结果表明:对于铱星和全球星系统,随着纬度降低,卫星可见数减小,多普勒几何精度因子变大;多普勒定位结果精度同时受到频率测量精度、卫星位置误差以及卫星速度误差影响,当卫星位置误差小于10 m、卫星速度误差小于0.1 km·s-1时,对定位结果影响不大,此时频率测量精度成为影响定位精度的决定性因素,且当频率测量精度为0.01 Hz时,定位精度可达1.18 m. 相似文献
16.
Glenn S. Orton 《Icarus》1977,32(1):41-57
The mean thermal structure of the Jovian atmosphere near the temperature minimum (0.1 bar) is recovered by inversion of thermal radiance data. Improvements over previous studies of this type are made in two respects. (1) Care is taken to select data sources which are on a consistent calibration scale and from a frequency region which minimizes the variance in the recovered temperature. (2) The accuracy in the temperature recovery vs the vertical resolution capability is studied quantitatively. The contributions of various sources of systematic error, which generate significant uncertainty in the recovered thermal structure, are assessed. Sources of systematic error include assumptions about the stratospheric NLTE source function, the extent of cloud cover, the methane mixing ratio, and the calibration scale. Future investigations are outlined which would reduce such uncertainties and provide consistency with a wider range of data on the Jovian upper atmosphere. 相似文献
17.
针对大口径、高性能射电望远镜天线受到的随机及时变风扰的问题, 利用自回归滑动平均模型预测望远镜周围风速, 提前计算风致结构变形量, 同时为望远镜伺服控制系统提供足够执行时间来降低风扰影响. 基于新疆奇台110m口径全向可动射电望远镜(QiTai Telescope, QTT)台址风场数据特征, 通过赤池信息准则和贝叶斯信息准则辨识模型阶次, 利用最大似然法估计模型参数, 分析模型残差特性以检验自回归滑动平均模型的有效性. 通过计算不同季度预测数据与测试数据偏差得到预测模型的精度, 夏季平均绝对误差为0.133mcdots-1, 秋季平均绝对误差为0.162mcdots-1, 冬季平均绝对误差为0.287mcdots-1. 整体来看, 基于QTT台址不同季度风速数据建立的自回归滑动平均模型预测误差较小, 满足射电望远镜风扰控制系统的需求, 能为大口径射电望远镜风扰控制提供必要数据支撑. 相似文献
18.
O. Groussin J. Licandro J. Helbert J. L. Reynaud P. Levacher M. Reyes García-Talavera V. Alí-Lagoa P. E. Blanc E. Brageot B. Davidsson M. Delbó M. Deleuze A. Delsanti J. J. Diaz Garcia K. Dohlen D. Ferrand S. F. Green L. Jorda E. Joven Álvarez J. Knollenberg E. Kührt P. Lamy E. Lellouch J. Le Merrer B. Marty G. Mas C. Rossin B. Rozitis J. Sunshine P. Vernazza S. Vives 《Experimental Astronomy》2016,41(1-2):95-115
We present THERMAP, a mid-infrared spectro-imager for space missions to small bodies in the inner solar system, developed in the framework of the MarcoPolo-R asteroid sample return mission. THERMAP is very well suited to characterize the surface thermal environment of a NEO and to map its surface composition. The instrument has two channels, one for imaging and one for spectroscopy: it is both a thermal camera with full 2D imaging capabilities and a slit spectrometer. THERMAP takes advantage of the recent technological developments of uncooled microbolometer arrays, sensitive in the mid-infrared spectral range. THERMAP can acquire thermal images (8–18 μm) of the surface and perform absolute temperature measurements with a precision better than 3.5 K above 200 K. THERMAP can acquire mid-infrared spectra (8–16 μm) of the surface with a spectral resolution Δλ of 0.3 μm. For surface temperatures above 350 K, spectra have a signal-to-noise ratio >60 in the spectral range 9–13 μm where most emission features occur. 相似文献
19.
Long-term Clock Bias Prediction Based on An ARMA Model 总被引：1，自引：0，他引：1
XI Chao CAI Cheng-lin LI Si-min LI Xiao-hui LI Zhi-bin DENG Ke-qun 《Chinese Astronomy and Astrophysics》2014
The long-term and reliable prediction of satellite clock bias (SCB) is an important prerequisite for realizing the satellite autonomous navigation and orbit determination. Considering the shortcomings of the quadratic polynomial model (PM) and gray system model (GM) in the long-term prediction of SCB, a new prediction method of SCB based on an ARMA (Auto-Regressive Moving Average) model is proposed to represent the variation characteristics of SCB more accurately. In this paper, a careful precision analysis of the 90-day SCB prediction is made to verify the feasibility and validity of this proposed method by using the IGS (International GNSS Service) clock data. According to the variation characteristics of each satellite clock, the pattern recognition, modeling and prediction of SCB are conducted, and the detailed comparison is made with the other three models at the same time. The results show that adopting the ARMA model can effectively improve the accuracy of long-term SCB prediction. 相似文献