高精度混合型格式的构造及数值模拟

在守恒变量形式的无波动无自由参数耗散(NND)格式的基础上,引入样条插值的思想,并采用具有一致二阶精度格式的限制器函数,构造了一个在光滑区具有四阶精度,在激波附近降为二阶精度的混合型格式。在计算中采用具有总变差减少(TVD)性质的四阶R unge-K u tta方法进行时间离散,通过对多个典型算例的计算,并与NND格式作了比较,分析结果表明:混合四阶格式引起的耗散和波动较小,并且能够高精度地分辨间断。     

电弧风洞喷管壁温对平板试验的影响研究

为研究电弧风洞喷管壁面温度对平板试验的影响,研制了隔热半椭圆喷管,采用电弧风洞半椭圆喷管平板试验的方法,将喷管长轴边与平板试验模型连接,使气流延伸到模型表面进行试验。喷管扩张段水冷壁面在试验初始时期（冷壁）和壁温上升（热壁）条件下,试验研究了平板测试模型表面冷壁热流和平衡温度的变化。结果表明：在喷管来流焓值1.00～2.55 MJ/kg范围内,相对于冷壁,热壁模型表面冷壁热流增加4.7%～15.0%,平衡温度最大升高4.24%。因此,热防护试验时应考虑喷管壁面温度对平板试验结果带来的影响,需要提高来流焓值。

     

A robotic telescope network for space debris identification and tracking

The two TAROT (Télescopes à Action Rapide pour les Objets Transitoires; Rapid Action Telescopes for Transient Objects) installations are fully robotic optical observatories with optimized observation scheduling, data processing and archiving. Zadko is a 1 m telescope in Western Australia. The fully robotisation of the Zadko telescope has just been completed; it is now included in the TAROT network. In this paper we provide an overview of this international network of robotic optical telescopes. We discuss the advantages of using the network to participate in a satellite and space debris tracking program. This network will access almost all geostationary belt objects, and provide the first real-time satellite positioning capability. The inclusion of the 1 m Zadko telescope into the network significantly extends the efficiency and sensitivity of the existing two telescope configuration.     

超高速碰撞碎片散布数值分析

基于光滑粒子流体动力学(SPH)方法,对低轨卫星与某空间物体的超高速碰撞问题进行了数值模拟。通过确立航天器轨道高低判定准则及判定方法,分析了碰撞角度、碰撞速度对碰撞碎片散布的影响情况。仿真结果表明,低轨卫星与空间物体碰撞产生的大部分空间碎片所处轨道高度位于原卫星轨道周围;碰撞碎片的散布情况与碰撞方式密切相关,相比于上升式碰撞,下压式碰撞产生的下降碎片个数较多,上升碎片个数较少;低轨卫星与空间物体碰撞产生的空间碎片总数与碰撞相对速度密切相关,碰撞相对速度越大,碎片数量越多;随着碰撞相对速度的增大,上升碎片、下降碎片及双曲碎片的个数逐渐增加;在不改变碰撞总动量数量级的条件下,改变空间物体的速度大小对空间碎片散布的影响并不明显。     

Variations of total electron content over high latitude region during the ascending phase of 24th solar cycle

The solar cycle variation and seasonal changes significantly affects the ionization process of earth’s ionosphere and required to be monitored in real time basis for regional level refinement of existing models. In view of this, the present study has been carried out by using the ionospheric Total Electron Content (TEC) data observed with the help of Global Ionospheric Scintillation and TEC monitoring (GISTM) system installed at Indian Antarctic Research Station, “Maitri” [70°46′00″S 11°43′56″E] during the ascending phase of 24th solar cycle. The daily values of solar extreme ultraviolet (EUV) flux (0.1–50?nm wavelength), 10.7?cm radio flux F_10.7 and Sunspot number (SSN) has been taken as a proxy to represent the solar cycle variation to correlate with TEC. The linear regression results revels better correlation of TEC with EUV flux rather than F_10.7 and SSN. Also, the EUV and TEC show better agreement during summer as compared to winter and equinox period. Correlation between TEC and EUV appears significantly noticeable during ten internationally defined quiet days of each month (stable background geophysical condition) as compared to the overall days (2010–2014). Further, saturation effect has been observed on TEC values during the solar maxima year 2014. The saturation effects are more prominent during the night hours of winter and equinox season due to transportation losses manifested by the equator-ward direction of meridional wind.     

Apparent rotation properties of space debris extracted from photometric measurements

Knowledge about the rotation properties of space debris objects is essential for the active debris removal missions, accurate re-entry predictions and to investigate the long-term effects of the space environment on the attitude motion change. Different orbital regions and object’s physical properties lead to different attitude states and their change over time.Since 2007 the Astronomical Institute of the University of Bern (AIUB) performs photometric measurements of space debris objects. To June 2016 almost 2000 light curves of more than 400 individual objects have been acquired and processed. These objects are situated in all orbital regions, from low Earth orbit (LEO), via global navigation systems orbits and high eccentricity orbit (HEO), to geosynchronous Earth orbit (GEO). All types of objects were observed including the non-functional spacecraft, rocket bodies, fragmentation debris and uncorrelated objects discovered during dedicated surveys. For data acquisition, we used the 1-meter Zimmerwald Laser and Astrometry Telescope (ZIMLAT) at the Swiss Optical Ground Station and Geodynamics Observatory Zimmerwald, Switzerland. We applied our own method of phase-diagram reconstruction to extract the apparent rotation period from the light curve. Presented is the AIUB’s light curve database and the obtained rotation properties of space debris as a function of object type and orbit.     

Post-Newtonian tracking formulae to increase the shooting accuracy of autonomous LEO laser trackers

We introduce five post-Newtonian tracking formulae that would allow increasing the accuracy of the shooting systems on board autonomous LEO laser trackers. These formulae should be used when the current formulae cannot provide instants close enough to the optimal instants at which the trackers could safely shoot down unwished LEO middle-distant targets. In fact, they allow the trackers to produce not only the safest shooting actions, but also the most efficient ablations that might make the targets fall into the atmosphere for them to burn. The fact of the matter is in the falsifiability procedure introduced below, which allows to simulate sequences of unharming shooting actions with very narrow laser beams leading to identify the optimal pointing directions to previously selected debris objects whose size and composition are representative of these targets.     

证券市场资金流量模型研究

证券市场证券价格的运动可以划分为有明确趋势的定向运动与无趋势的随机波动。证券价格定向运动产生的内在原因及运动规律,是研究证券投资最关心的重要问题。文章以股票市场作为研究对象,从场内存量资金的定量分析着手,研究导致股价做定向运动的资金流量原理及其相关模型,得出资金进出股市“净流入（出）量”的测度方法履系列结论。