月球探测器自主软着陆中的三维重构技术研究

为了使月球探测器自主的在月球表面进行软着陆，应对着陆区域的地形进行三维重构的方法，获得着陆区域的地形描述。提出了一种通过运动获得长基线的立体视觉的三维重构方法，针对长基线立体视觉方法所存在的问题，通过设计一系列的算法，完成了图像特征点选取和匹配，估计相机在不同位置的相对旋转和位移；对立体图像对进行校正，获得稠密的视差图；通过视差图进行三维重构，生成着陆区域的DEM。根据月球地形的特点建立了软件仿真平台，并且在仿真平台的基础上对文中的算法进行验证。仿真的结果表明该方法可以有效的应用于月面地形的三维重构。     

In-orbit operation and performance of the CubeSat Soft X-ray polarimeter PolarLight

PolarLight is a compact soft X-ray polarimeter onboard a CubeSat, which was launched into a low-Earth orbit on October 29, 2018. In March 2019, PolarLight started full operation, and since then, regular observations with the Crab nebula, Sco X-1, and background regions have been conducted. Here we report the operation, calibration, and performance of PolarLight in the orbit. Based on these, we discuss how one can run a low-cost, shared CubeSat for space astronomy, and how CubeSats can play a role in modern space astronomy for technical demonstration, science observations, and student training.     

复杂群塔风荷载试验研究

介绍了一复杂群塔结构节段刚性测压试验概况和主要试验结果,讨论了结构典型部位风压分布的基本特征和结构风压分布的基本规律.试验结果表明,由于该结构由多个单体高耸塔结构组成,相互干扰严重,风压的分布相当复杂.根据风压试验结果得到了风力沿各塔高度的分布,并讨论了分布规律,进一步得出基底剪力系数和基底弯矩系数,分析了最危险风向,给出了用于结构设计的荷载建议.     

嫦娥五号平动点拓展任务轨道方案研究

中国嫦娥五号探测器成功实现月球采样返回任务,为最大限度利用任务资源,研究了利用嫦娥五号轨道器的平动点拓展任务轨道方案,设计了平动点轨道及其转移轨道.首先,给出了任务轨道设计的轨道动力学模型,包括圆型限制性三体问题模型和精确力模型.其次,基于嫦娥二号和嫦娥5T1平动点拓展任务设计经验,介绍了平动点轨道直接转移与入轨等轨道...     

基于蜕变 Voronoi 多边形的扇区优化方法

根据空域中航路点的自然分布 ,利用算法几何的思想建立Voronoi图 ,并依照空域划分的原则将由Voronoi图获得的单元蜕变 ,统计由各蜕变Voronoi多边形构成的有限元内包含的管制员工作负荷。然后以工作负荷均衡为优化原则 ,使用模拟退火算法对空域中的有限元进行优化组合 ,新解要求满足空域划分的 2个原则的约束。这样 ,有限元组合集合的边界就是优化的扇区边界。通过实际空域设计算例的计算结果 ,验证本文提出的扇区优化方法的合理性。     

Analysis of precipitable water vapor from GPS measurements in Chengdu region: Distribution and evolution characteristics in autumn

The rainfall process of Chengdu region in autumn has obvious regional features. Especially, the night-time rain rate of this region in this season is very high in China. Studying the spatial distribution and temporal variation of regional atmospheric precipitable water vapor (PWV) is important for our understanding of water vapor related processes, such as rainfall, evaporation, convective activity, among others in this area. Since GPS detection technology has the unique characteristics, such as all-weather, high accuracy, high spatial and temporal resolution as well as low cost, tracking and monitoring techniques on water vapor has achieved rapid developments in recent years. With GPS–PWV data at 30-min interval gathered from six GPS observational stations in Chengdu region in two autumns (September 2007–December 2007 and September 2008–December 2008), it is revealed that negative correlations exist between seasonally averaged value of GPS–PWV as well as its variation amplitude and local terrain altitude. The variation of PWV in the upper atmosphere of this region results from the water vapor variation from surface to 850 hPa. With the help of Fast Fourier Transform (FFT), it is found that the autumn PWV in Chengdu region has a multi-scale feature, which includes a seasonal cycle, 22.5 days period (quasi-tri-weekly oscillation). The variation of the GPS–PWV is related to periodical change in the transmitting of the water vapor caused by zonal and meridional wind strengths’ change and to the East Asian monsoon system. According to seasonal variation characteristics, we concluded that the middle October is the critical turning point in PWV content. On a shorter time scale, the relationship between autumn PWV and ground meteorological elements was obtained using the composite analysis approach.     

Space Debris Research Activities In China In 2007

The year 2007 was important for us to carry out the Eleventh Five-Year Space Debris Research Action Plan.Through the unremitting efforts of all space debris project research groups,we completed the space debris research projects in 2007 successfully,among which we made the substantive progress in many projects, which has laid a good foundation for the continuous research in the future.     

飞船自主应急返回控制参数确定方法及应用

当飞船在无地面测控支持的运行段飞行时,必须考虑故障情况下飞船自主返回应急着陆区的控制参数确定问题。本文根据飞船自主应急返回的主要特点和应急着陆区的选取原则,在分析飞船再入动力学过程和实际测量数据的基础上,确立了一种飞船自主应急返回的控制参数计算方法及流程,并简要介绍了该方法在“神舟4号”等飞船测控任务中的应用。     

洛氏硬度标准装置不确定度的评定

详细给出了洛氏硬度标准装置不确定度的评定方法及步骤。     

New split-winding doubly salient permanent magnet motor drive

A new split-winding doubly salient permanent magnet (DSPM) motor drive is proposed. This DSPM motor drive offers the advantages of high power density, high efficiency, and wide speed range. The corresponding operation, analysis, implementation, and experimentation are successively presented. Finally, experimental results are used to confirm that the proposed DSPM motor drive offers high efficiency over a wide output power range, exhibits good dynamic performance, and extends the constant-power operation range significantly.