载人航天器低空应急救生分离时刻计算

讨论了载人航天器低空应急救生时返回舱与逃逸飞行器分离时刻Ｔａ的计算方法。首先推导了逃逸弹道的近似解;然后提出了基于近似解的返回舱与逃逸飞行器分离时刻Ｔａ的实时确定方法;最后,仿真分析了该方法对提高载人航天器低空逃逸救生概率的作用,证明利用近似解实时求解分离时间Ｔａ是一种简单实用、效果明显的方法。     

民用飞机电子设备舱推力回收喷管计算分析

介绍了某型民用飞机电子设备舱排气系统主要组成,排气系统推力回收喷管的工作原理和设计要求,并分别通过理论计算和CFD三维仿真模拟,验证了该推力回收喷管的性能和关键设计尺寸。     

国内外深空探测器精密定轨软件研究综述及WUDOGS简介

深空探测器精密定轨软件系统的研制在深空探测活动中是一个非常重要的环节,一直受到各大航天机构的重视。针对国内外深空探测器精密定轨软件平台的研究现状,重点介绍了具有代表性的美国JPL(Jet Propulsion Laboratory,喷气推进实验室)的DPTRAJ/ODP(Double Precision TRAJectory program/Orbit Determination Program,双精度轨道程序/定轨程序)和MONTE(Mission analysis,Operations,and Navigation Toolkit Environment,任务分析、操作和导航工具箱环境),GSFC(Goddard Space Flight Center,戈达德航天飞行中心)的GEODYN-II以及法国CNES(Centre National dEtudes Spatiales,国家空间研究中心)的GINS(Géodésie par Intégrations Numériques Simultanées,同步数值积分大地测量)软件系统,对这些软件的结构与功能进行了总结。之后对武汉大学自主研制的深空探测器精密定轨软件系统WUDOGS(Wuhan University Deep space Orbit determination and Gravity recovery System,武汉大学深空探测器精密定轨与重力场解算软件系统)的主要模块与功能进行了介绍,通过与GEODYN-II的交叉对比验证,表明:对于探测器的轨道预报,WUDOGS与GEODYN-II的1个月位置差异小于0.3mm,2d位置差值小于5×10~(-3) mm;双程测距、双程测速的理论计算值和GEODYN-II的差值RMS(Root Mean Square,均方根)分别在0.06mm,0.002mm/s的水平;WUDOGS目前已初步具备了月球和火星探测器精密定轨能力。最后对WUDOGS的下一步发展方向进行了展望。     

高速旋板泵旋板动压支承设计

旋板端部与定子内表面间的摩擦副设计是高速旋板泵设计的技术关键。本文把流体动力润滑理论用于高速旋板泵的设计,着重探索旋板动压支承的设计,提出了一种设计方法。算例结果表明,本文的设计方法可使动压支承尺寸与泵总体尺寸相匹配。     

运载火箭助推器回收技术分析与启示

可重复使用运载火箭对于实现低成本、高可靠、自由进出空间具有重要作用,是提高我国进入空间能力,提升我国综合国力的重要途径之一,实现助推器回收是运载火箭进行重复使用的核心技术。以运载火箭可重复使用技术为背景,从运载火箭助推器伞降回收、垂直返回和带翼飞回3种回收方式着手,充分调研了美国、俄罗斯、欧洲在运载火箭助推器回收技术领域开展的几个典型项目的方案特点和研制情况,以及我国相关技术的发展状况,分析比较其技术难点和应用前景,提出我国发展助推器回收技术的相关建议,为我国发展可重复使用运载火箭提供研究发展思路和参考。     

Precessing motion in stratified radial swirl flow

Vortex/flame interaction is an important mechanism for unsteady combustion in a swirl combustion system. Technology of low emission stirred swirl(Te LESS), which is characterized with stratified swirl flow, has been developed in Beihang University to reduce NOXemission. However,large-scale flow structure would be induced in strong swirl flow. Experiments and computational fluid dynamics(CFD) simulation were carried out to investigate the unsteady flow feature and its mechanism in Te LESS combustor. Hotwire was firstly applied to testing the unsteady flow feature and a distinct mode with 2244 Hz oscillation frequency occurred at the pilot swirl outlet.The flow mode amplitude decayed convectively. Large eddy simulation(LES) was then applied to predicting this flow mode and know about its mechanism. The deviation of mode prediction compared with hotwire test was 0.8%. The spiral isobaric structure in pilot flow passage indicates that precessing vortex core(PVC) existed. The velocity spectrum and phase lag analysis suggest that the periodic movement at the pilot outlet was dominated by precessing movement. Negative tangential momentum gradient reflects that the swirl flow was unstable. Another phenomenon was found out that the PVC movement was intermittently rotated along the symmetric axis.     

基于Rician分布的SAR图像MRG目标提取算法

针对SAR图像特有的乘性噪声和非恒虚警统计特性很难正确提取目标的问题,本文提出了MRG算法对SAR目标进行检测。首先用MRF-ICM算法对SAR图像进行后向散射系数的复原,再在复原后的幅度上叠加相位信息后引入Rician分布寻找自适应的最佳局域Gabor滤波器参数对SAR图像进行目标提取。和以往的算法相比,MRG算法充分利用了SAR图像幅度和相位中所携带的信息,能更准确地提取目标。实验表明:该方法能取得很好的目标检测效果,后期提取出的目标更符合实际目标形态,具有较强的通用性。     

网络数据包还原和内容分析系统的设计与实现

设计并实现了面向内容安全的局域网监控系统。该系统包括网络数据内容还原和内容分析与过滤两大模块,采用旁听模式捕获网络数据包,利用协议分析和会话还原技术实现了应用数据还原;通过文本分析和过滤技术对还原后的应用数据进行安全性检验。该系统能够进行网络信息实时监控,有效地实现了局域网的信息内容监管。     

On the selection of optimal global geopotential model for geoid modeling: A case study in Pakistan

A statistical comparison has been made between gravity field parameters derived from different global geopotential models (GGMs) and observed gravity anomalies, gravimetric geoid and GPS-Leveling data. The motivation behind this study is the selection of best possible global geopotential model that best matches statistically with the local observed data in Pakistan. This will facilitate in decreasing the load on observed data for the development of regional gravimetric geoid in remove-compute-restore technique when used in the Stokes’s integral for computation of the residual part. It is observed that combined geopotential models such as EGM96 and PGM200A, EIGEN-GL04C and EIGEN-CG03C reflect the better match in the total spectral range of gravity and GPS-Leveling data. Results of the precise local geoid model also indicate similar characteristics. A very-high-degree model “EGM2008” (degree/order 2160) exhibits relatively superior statistical fit with observed ground data in Pakistan region. For satellite-only models an increasing trend in the standard deviation can be seen with maximum of about ∼4 m in difference between GPS-Leveling and corresponding GGM’s geoid with increase in the order from 50 to 120 and then it decreases afterwards. However, for the EIGEN-CHAMP03SP, standard deviation saturates to a value of 3.4 m. This is an indication of contamination in the long to medium wavelength part, i.e. 50–100° for the satellite-only models. Moreover, the models DEOS-CHAMP-01C, GGM02C and then ITG-GRACE03 appear to have better fit for medium to long wavelength and can possibly be recommended for use as long wavelength part with the local observed data. While a hybrid geopotential model selection can be achieved through the selection from either of DEOS-CHAMP-01C, GGM02C, GGM02S, EIGEN-GRACE02S or ITG-GRACE03 in the long wavelength (to degree and order 40) and EGM96, PGM200A, EIGEN-GL04C, EIGEN-CG03C or even EGM2008 in medium to short wavelength, i.e. from degree 41 to maximum degree and order.     

实时高可用测控集群关键技术研究

针对实时测控信息类型复杂、信息处理和控制方法多样、对实时性和可靠性要求高等特点,构建了一种基于集群计算平台的实时、高可用测控系统,在此基础上提出了一主一备双工热备节点的分布式集群管理控制模式,即在系统运行过程中任务除在一个节点上进行处理外,另一节点同时运行该任务处理(但不输出处理结果),在此基础上设计了任务故障监测的心跳机制、任务故障迁移和恢复的分配方法。通过实验证明,该方法能在一个处理周期内发现任务故障,并实现故障任务的迁移和恢复,不仅减少了系统建设成本,而且缩短了故障任务迁移和恢复时间,提高了测控系统的实时性、可靠性。