导航卫星的单星定轨

本文对导航卫星的单星定轨进行了初步探讨，针对单星定轨时卫星钟钟差和接收机钟钟差难以处理的特点，提出了定轨的同时解算测站距离偏差和采用平均距离变化率进行定轨两种方案，采用GPS的实测数据试验计算表明，两种计算方案均能初步完成单星定轨任务。     

基于WRF数值模拟的夏季强对流测定方法研究

在固定时间内使WRF数值模式的预报和观测间距实现最小化,是实时准确测定夏季强对流的重要依据,因此研究一种基于WRF数值模拟的夏季强对流测定方法.通过分析河南省2018年7月2日至7月23日闪电定位资料和降水资料,统计夏季强对流天气中降水强度与闪电频数关系,将二者进行线性拟合,根据拟合结果将夏季强对流天气中闪电频数反演至降水强度,并将反演后的降水强度通过四维变分同化资料方法,同化至WRF数值模拟中,获取最终WRF极小化代价函数,实现夏季强对流天气实时准确测定.通过该方法对河南省某机场进行WRF数值模拟研究发现,模拟结果的水平风速、垂直速度、位温与扰动气压变化明显,可准确测定该机场的夏季强对流天气,具有可靠性.     

The impact of accelerometry on CHAMP orbit determination

 The contribution of the STAR accelerometer to the CHAMP orbit precision is evaluated and quantified by means of the following results: orbital fit to the satellite laser ranging (SLR) observations, GPS reduced-dynamic vs SLR dynamic orbit comparisons, and comparison of the measured to the modeled non-gravitational accelerations (atmospheric drag in particular). In each of the four test periods in 2001, five CHAMP arcs of 2 days' length were analyzed. The mean RMS-of-fit of the SLR observations of the orbits computed with STAR data or the non-gravitational force model were 11 and 24 cm, respectively. If the accelerometer calibration parameters are not known at least at the few percent level, the SLR orbit fit deteriorates. This was tested by applying a 10% error to the along-track scale factor of the accelerometer, which increased the SLR RMS-of-fit on average to 17 cm. Reference orbits were computed employing the reduced-dynamic technique with GPS tracking data. This technique yields the most accurate orbit positions thanks to the estimation of a large number of empirical accelerations, which compensate for dynamic modeling errors. Comparison of the SLR orbits, computed with STAR data or the non-gravitational force model, to the GPS-based orbits showed that the SLR orbits employing accelerometer observations are twice as accurate. Finally, comparison of measured to modeled accelerations showed that the level of geomagnetic activity is highly correlated with the atmospheric drag model error, and that the largest errors occur around the geomagnetic poles. Received: 7 May 2002 / Accepted: 18 November 2002 Correspondence to: S. Bruinsma Acknowledgments. The TIGCM results were obtained from the CEDAR database. This study was supported by the Centre National d'Etudes Spatiales (CNES). The referees are thanked for their helpful remarks and suggestions.     

哌啶树脂在富集分离中应用研究——Ⅰ.岩石矿物中痕量银的分离富集及测定

本文采用410哌啶树脂分离岩石矿物中基体元素后富集痕量Ag。交换酸度为0.25—3.5mol/LHCl介质,树脂柱上的Ag用热的0.5—1.0％硫脲解脱,并以火焰原子吸收法测定。方法简便、快速,用于岩矿中痕量Ag的富集和测定结果满意。     

Fast sequential indicator simulation: Beyond reproduction of indicator variograms

Sequential Indicator Simulation (SIS), although widely used, is relatively slow, and requires tedious inference of a large number of indicator variogram models. SIS is designed only to estimate class proportions and to reproduce indicator variogram models; the statistics of the continuous attribute being simulated,z-histogram and variogram, may be poorly reproduced. Several implementations of the SIS algorithm are proposed resulting in better reproduction of statistics yet with better CPU performance.     

A projective approach to orbit determination from three sight-lines

Concepts from projective geometry are used to provide a coherent framework for the determination of orbits from observation data comprising lines of sight at three known times. A novel way of presenting the results in a finite diagram is introduced, The effectiveness of the approach is demonstrated by an example, using a simple spreadsheet. A computer-graphic implementation is recommended.     

Modelling and distance determination of planetary nebulae

At present the lack of a good, generally accepted distance scale is the major limitation in the study of Planetary Nebula (PN) evolution and their distribution. We describe our fully self-consistent method to derive the physical parameters of a PN, including its distance, from a set of observables. For this we calculate various models and search for a best fit of the model predictions to the observables. An accurate determination of the angular diameter is important for a good distance determination. We think that we shall achieve an accuracy of 30% in distance. We estimate the error in stellar temperature at less than 15% and the uncertainty in the abundances at 0.10 dex.     

北斗卫星ECOM光压模型参数选择策略分析

以ECOM经验光压模型为基础,利用北斗卫星3年的精密星历进行轨道拟合,获得了ECOM光压参数的变化规律,给出了北斗3类卫星的ECOM光压参数选择策略。从北斗卫星姿态控制模式出发,通过卫星星体受照分析,指出在北斗卫星地影期零偏航状态下,由于太阳对卫星帆板的不正照,导致与动态偏航姿态相比,光压摄动力存在与轨道周期相关的分量,需要在ECOM 5参数的基础上增加D向周期分量进行吸收。通过MGEX全球网数据定轨试验,本文提出的方法可使零偏段定轨重叠段位置精度提高50%~80%。     

星地跟踪网的导航卫星精密轨道确定及预报

针对区域跟踪网不能覆盖导航卫星全弧段从而导致卫星定轨精度低的问题,简述了导航卫星和低轨卫星联合定轨模型,然后利用星地跟踪网观测数据同时确定了低轨卫星和导航卫星精密轨道,并根据实验结果详细分析了低轨卫星在联合定轨中所起到的作用。计算结果表明,引入低轨卫星之后,全球网和区域网定轨精度分别平均提高了20.0%和44.3%,区域网6h和24h的轨道预报精度分别优于10cm、13cm,利用星地跟踪网观测数据联合定轨方案是一种提高定轨精度并削弱对地面站依赖性的有效方法。     

星载GPS的多目标跟踪数据处理方法

针对测量船外测数据对多个目标进行定轨精度较低的问题,该文提出了星载GPS数据、测量船外测数据的融合处理方法。在多目标测控任务中,航天测量船船载设备获取的外测数据仅包含一个主跟踪目标的测角数据和多个跟踪目标的测距数据,且测角数据精度较低,该文采用由星载GPS数据获取的等效测角数据和由测量船外测设备获取的测距数据进行定轨,经过分析试算,该方法有效弥补了船载外测设备测角数据精度较低的问题,提高了初轨确定的能力以及卫星星间距离的解算精度。