Chang'E-1 Lunar Mission:An Overview and Primary Science Results

Chang'E-1 is the first lunar mission in China, which was successfully launched on Oct. 24th, 2007. It was guided to crash on the Moon on March 1, 2009, at 52.36ºE, 1.50ºS, in the north of Mare Fecunditatis. The total mission lasted 495 days, exceeding the designed life-span about four months. 1.37 Terabytes raw data was received from Chang'E-1. It was then processed into 4 Terabytes science data at different levels. A series of science results have been achieved by analyzing and applicating these data, especially "global image of the Moon of China's first lunar exploration mission'. Four scientific goals of Chang'E-1 have been achieved. It provides abundant materials for the research of lunar sciences and cosmochemistry. Meanwhile these results will serve for China's future lunar missions.     

钎焊气氛对金刚石磨粒与钎料界面微观结构的影响

在真空和Ar气两种不同的氛围中,采用NiCr合金钎料,进行了炉中钎焊金刚石磨粒的试验研究。运用扫描电镜（SEM）、X-射线能谱仪（EDS）和X-射线衍射结构研究了不同钎焊气氛对NiCr合金钎料成分和金刚石磨粒与钎料界面微观结构的影响。结果表明：（1）在不同的钎焊气氛下,由于氧分压的不同导致了NiCr合金钎料的成分也不相同。在Ar气保护气氛下的炉中钎焊金刚石试样表面有B2O3生成。（2）在不同钎焊气氛中,在金刚石磨粒与合金钎料界面生成物都主要为铬的碳化物。但生成物表面形貌不同,在真空炉中焊后的金刚石磨粒表面生成物成放射状生长,而在Ar气保护炉中钎焊后的金刚石磨粒表面生成物如杂草一样生长且生成物组织较真空炉中细小。     

1981年7月31日漠河地区日食的外电离层效应

本文利用漠河(磁径190°17′E, 磁纬42°18′N)地区接收的哨声和同时观测的电离层资料, 采用南北半球电子浓度不一定对称的假设, 以电离层垂测资料和哨声联合换算的模式法, 得到了1981年7月31日哨声色散常数的日食效应;并粗略地测定了日食期间, 漠河上空沿磁力线分布的电子浓度剖面, 磁通量管电子含量和等效标高的部分结果;此外, 还初步讨论了日食的外电离层效应.     

复合材料机翼结构力学性能仿真与验证研究

随着航空航天技术的发展和轻量化要求,复合材料在机翼上的应用比重日益增大。为研究复合材料机翼结构的力学性能,本文采用ABAQUS有限元软件建立了某型复合材料机翼的有限元模型,结合实际工况对机翼工艺结构进行仿真模拟。研究表明,仿真手段可极大提高研制效率,是机翼研制的有效工具;共固化工艺能够有效减少紧固件数量,进而降低由应力集中带来失效的风险。     

基于MOEA/D的三锥体拦截器气动外形优化设计

针对由临近空间拦截器飞行环境变化剧烈导致的热流密度过高等问题,提出一种多目标外形优化设计方法,并针对一种新型三锥体临近空间拦截器外形进行优化设计。首先,建立飞行器的气动、弹道、气动热等多学科分析模型,利用高斯-伪谱法计算拦截弹道,利用桥函数法建立气动模型,并利用Fay-Riddle方法估计气动热流密度。然后,以飞行器航程、总热流量和飞行时间为优化目标,采用基于分解的多目标进化算法(MOEA/D)与伪谱法将该问题转化为一组单目标优化子问题,得到Pareto前沿并进行相关分析。最后,给出一个优于基准值,同时满足性能指标要求的新型外形。结果表明:该优化方法具有可实现性,为未来的飞行器设计提供了新思路。     

有源集成背馈式接收天线设计

为了提高接收天线系统的增益以及灵敏度,对于天线与射频前端组成的接收系统采用了一种有源集成接收天线的设计方案,从而省略了传统设计中的有源电路与微带天线之间的匹配网络.依照此方案,设计并实现了一个背馈结构的矩形微带天线与前级低噪声放大器电路的有源集成.矩形微带天线的馈电点与低噪声放大器的输入端通过金属探针相连,当天线在2.48?GHz谐振时,通过选择合适的馈电点位置,天线产生放大器设计所需的输入阻抗.有源集成背馈式接收天线工作于S波段,最终的测试结果显示了其优良的特性.     

Design of tracking mount and controller for mobile satellite laser ranging system

In this study, we have proposed and implemented a design for the tracking mount and controller of the ARGO-M (Accurate Ranging system for Geodetic Observation - Mobile) which is a mobile satellite laser ranging (SLR) system developed by the Korea Astronomy and Space Science Institute (KASI) and Korea Institute of Machinery and Materials (KIMM). The tracking mount comprises a few core components such as bearings, driving motors and encoders. These components were selected as per the technical specifications for the tracking mount of the ARGO-M. A three-dimensional model of the tracking mount was designed. The frequency analysis of the model predicted that the first natural frequency of the designed tracking mount was high enough. The tracking controller is simulated using MATLAB/xPC Target to achieve the required pointing and tracking accuracy. In order to evaluate the system repeatability and tracking accuracy of the tracking mount, a prototype of the ARGO-M was fabricated, and repeatability tests were carried out using a laser interferometer. Tracking tests were conducted using the trajectories of low earth orbit (LEO) and high earth orbit (HEO) satellites. Based on the test results, it was confirmed that the prototype of the tracking mount and controller of the ARGO-M could achieve the required repeatability along with a tracking accuracy of less than 1 arcsec.     

基于KS函数的协同优化算法及其应用

多学科设计优化(MDO)是当前航空航天复杂系统设计研究中一个最新、最活跃的领域,针对多学科设计优化中协同算法优化过程中存在的收敛困难、计算量大、费时等问题,提出一种新的系统级约束处理方法,利用KS函数的凝聚特性,将系统级的多个学科约束凝聚成一个拥有光滑高阶可微的可行域单约束,来取代罚函数法中的多个约束,以缓解多约束之间的冲突并加速收敛速度.利用两个典型算例进行测试,结果表明改进方法有效.     

机场竞争力评价指标体系的构建

本文首先分析总结了机场竞争力的形成机理,在此基础上提出了机场竞争力的评价原则,最后,构建了一套包含4个一级指标、16个二级指标和41个三级指标的机场竞争力评价指标体系,旨在通过这套评价体系对机场的竞争力发展水平进行评估,找出机场竞争力发展过程中的优势不足,为机场在市场竞争中提高竞争力水平和核心竞争力提供科学的参考依据.