运载火箭弹性模态数据使用方法研究

针对新研制运载火箭型号的特点,改进传统弹性模态数据的使用方法,并按照改进后的弹性模态数据使用方法建立火箭动力学运动方程,设计控制系统参数后进行姿控系统仿真,分析火箭采用摆助推控制方案后姿控系统的稳定性,结果表明改进后的数学模型与相应的模态数据使用方法能够更真实地反映火箭的运动特性。     

操纵评分自动管理系统在机务系统的应用

研究一种新模式,对乘务员机车标准化作业、乘务员档案信息等进行自动管理、统计和考核,代替原有的人工模式,加强管理者对机务行车部门的管理,提高管理的效益和水平,同时也确保运用行车的安全,使机务系统信息化得到进一步提高。     

INTELLIGENT MECHANISM TO SUPPORT DFX-ABILITIES IN AUTOMATED DESIGNER''''S ENVIRONMENT

Asis well known,time,quality and cost havebeen the three key criteria of product competi-tiveness in the market,and now the focus isplacedon product development time reduction,fromwhich other metricsprobably can be obtained.Thewhole product design and development process iscarried out along the timeline of product life- cycle.At the stage of design decision making,70 % to80 % of the productlife cycle value is formed attheexpense of about2 0 % of productlife cycle[1] .So itwill be the mosteffec…     

The plasma sheet and boundary layers under northward IMF: A multi-point and multi-instrument perspective

During conditions of northward interplanetary magnetic field (IMF), the near-tail plasma sheet is known to become denser and cooler, and is described as the cold-dense plasma sheet (CDPS). While its source is likely the solar wind, the prominent penetration mechanisms are less clear. The two main candidates are solar wind direct capture via double high-latitude reconnection on the dayside and Kelvin–Helmholtz/diffusive processes at the flank magnetopause. This paper presents a case study on the formation of the CDPS utilizing a wide variety of space- and ground-based observations, but primarily from the Double Star and Polar spacecraft on December 5th, 2004. The pertinent observations can be summarized as follows: TC-1 observes quasi-periodic (∼2 min period) cold-dense boundary layer (compared to a hot-tenuous plasma sheet) signatures interspersed with magnetosheath plasma at the dusk flank magnetopause near the dawn-dusk terminator. Analysis of this region suggests the boundary to be Kelvin–Helmholtz unstable and that plasma transport is ongoing across the boundary. At the same time, IMAGE spacecraft and ground based SuperDARN measurements provide evidence of high-latitude reconnection in both hemispheres. The Polar spacecraft, located in the southern hemisphere afternoon sector, sunward of TC-1, observes a persistent boundary layer with no obvious signature of boundary waves. The plasma is of a similar appearance to that observed by TC-1 inside the boundary layer further down the dusk flank, and by TC-2 in the near-Earth magnetotail. We present comparisons of electron phase space distributions between the spacecraft. Although the dayside boundary layer at Polar is most likely formed via double high-altitude reconnection, and is somewhat comparable to the flank boundary layer at Double Star, some differences argue in favour of additional transport that augment solar wind plasma entry into the tail regions.     

Java SDAI Study and Implementation

为了在Internet网上共享产品数据 ,基于Java语言实现了STEP标准数据读取接口SDAI.该实现包括几个部分 :EXPRESS信息模型向Java语言的映射 ,JavaSDAI会话模式的实现和JOS Part2 1文件、JOS STEP数据库两个映射 .基于该JavaSDAI接口的STEP应用系统 ,可采用Browser Server三层体系结构 ,客户端用户通过通用的Internet网浏览器即可操作异地的STEP产品数据 ,该JavaSDAI接口既与Part 2 1文件又与关系型数据库 (SQLServer)相连接 .通过一个演示实例 ,对JavaSDAI的优、缺点进行了总结     

Energetic oxygen ions in the magnetosheath in the negative BZ phase of the CME on January 10, 1997

Energetic oxygen ion flux intensifications were observed by the HEP/LD instrument on board the GEOTAIL satellite thoughout the Bz negative phase of the CME event on January 10, 1997. At this time, the spacecraft was moving in the magnetosheath at 1500 LT on a magnetopause skimming segment of its orbit. The very steady southward magnetic field in the magnetosheath (negative Bz of the CME) was highly inclined forming an angle of 45° with respect to the north direction. The observed oxygen enhancements in the magnetosheath show anisotropic angular distributions which occupy a varying fraction of the unit sphere. These distributions became particularly narrow during the passage of a solar wind pressure pulse between between 1050 and 1113 UT. The details of the angular distributions in the magnetosheath favour a leakage model, although the reconnection model cannot be denied.     

一种带状加载宽缝超宽带天线设计研究

设计了共面波导馈电的圆形宽缝超宽带天线.该天线由宽缝天线变形而来,在3CHz～12GHz的工作频带范围内,具有平面小型化超宽带特性.通过带状加载圆形缝隙的方法,改善了此天线的辐射方向图特性.为了阻止其他通信系统对超宽带系统的干扰,设计时采用开路枝节获得陷波性能.采用基于时域有限积分法的CST MWS电磁仿真软件进行分析计算,表明该天线具有超宽带阻抗带宽特性,良好的辐射方向图带宽和增益平坦度.天线的测量结果与仿真值保持一致,能够满足超宽带通信系统应用要求.     

针刺预制体参数对C/C复合材料力学性能的影响

通过针刺与化学气相沉积分别制备碳纤维预制体与碳基体,获得针刺C/C复合材料.研究了针刺密度、针刺深度、网胎面密度等预制体成型工艺参数对C/C复合材料力学性能的影响,并探讨了预制体体积密度与C/C复合材料力学性能关联关系.结果表明,针刺密度在20～ 50针/cm2之间时,C/C复合材料拉伸强度先增后减,而层间剪切强度一直上升;针刺深度在10～16 mm之间时,拉伸强度和层间剪切强度随针刺深度的提高而增加;网胎面密度在100～300 g/m2之间时,拉伸强度和层间剪切强度随网胎面密度的提高而降低;当只改变针刺密度、针刺深度、网胎面密度其中一个成型参数时,拉伸强度和层间剪切强度受预制体密度影响显著,预制体密度可作为预测C/C复合材料力学性能的一个宏观成型参数.     

Chinese Space Experts Awarded with Honors at IAC

On October 3 – 7, the 62nd International Astronautical Congress (IAC) was held in Cape Town,South Africa. Chinese aerospace expert Liu Jiyuan was given the Von Karman Award, the highest such prize presented by the International Academy of Astronautics (IAA). Liu Jiyuan is the first Chinese     

基于5阶精度格式WCNS-E-5的p-multigrid方法研究

p-multigrid方法的基本思想是:在保证收敛结果为高阶精度的同时,利用低阶精度格式耗散大的特点,来改善高精度有限差分格式在迭代计算时收敛速度慢的弱点.本文基于5阶精度WCNS-E-5差分格式,引入1阶精度迎风格式和3阶精度加权格式,构造了p-multigrid方法,在迭代过程中采用了V循环、W循环、S循环、PreV和FMG循环等不同方式来应用这三种格式,并通过典型算例考察了这些循环方式对收敛速度的影响,初步数值试验表明,采用恰当的循环方式,本文所设计的p-multigrid方法能够加快收敛速度,并保证了最终收敛结果与5阶精度WCNS-E-5差分格式的一致性.