UNAMID: an African solution to a complex case of geopolitical dynamics

This article examines the geopolitical dynamics associated with the African Union (AU) and United Nations hybrid operation in Darfur (UNAMID) from the start of the Darfur conflict in 2003 until the time when UNAMID became fully operational in 2011. It provides an overview of the complex forces and geopolitical dynamics that affected the deployment of UNAMID and shaped its unique hybrid character. It mainly highlights those primary geopolitical factors that hindered the full deployment of UNAMID. It is concluded that this period was a showcase for the newly established AU and its support for its member states, as well as a new approach for the international community to maintain international peace and security in alliance with regional organisations.     

一种面向宽带复杂信号侦察的可配置计算应用框架

可配置计算系统的优势与系统设计过程的复杂性是一对矛盾,可配置计算框架为此提供了有益的思路。但受限于适用范围与通用性考虑,已有的特别是商业框架仅支持系统的静态重构。本文针对宽带信号侦察这一特定应用领域,提出了一种功能级可配置计算应用框架BSRRCS-RCAF,该框架将领域应用中具有共性的计算与功能模块抽取和集中起来,形成二进制比特流配置文件库,并提供构建此类系统的公共服务体系。基于公共服务体系以及配置文件库,当需要修改或者重新构建宽带信号侦察系统时,只需在现有框架下动态调用配置组件库,或者遵循框架的统一设计接口完善补充组件库中的特定功能部分,整个系统设计框架将得到方便复用,便于实现基于快速重构的多种系统功能。     

基于CPU-GPU混合计算平台的RNA二级结构预测算法并行化研究

RNA二级结构预测是生物信息学领域重要的研究方向,基于最小自由能模型的Zuker算法是目前该领域最典型使用最广泛的算法之一。本文基于CPU GPU的混合计算平台实现了对Zuker算法的并行和加速。根据CPU和GPU计算性能的差异,通过合理的任务分配策略,实现二者之间的并行协作计算和处理单元间的负载平衡;针对CPU和GPU的不同硬件特性,对Zuker算法在CPU和GPU上的实现分别采取了不同的并行优化方法,提高了混合加速系统的计算性能。实验结果表明,CPU处理单元在混合系统中承担了14%以上的计算任务,与传统的多核CPU并行方案相比,采用混合并行加速方法可获得15.93的全局加速比;与最优的单纯GPU加速方案相比,可获得16%的性能提升,并且该混合计算方案可用于对其它生物信息学序列分析应用的并行和加速。     

Analysis on damage characteristics and detonation performance of solid rocket engine charge subjected to jet

To further explore the damage characteristics and impact response of the shaped charge to the solid rocket engine (SRE) in storage or transportation, protective armor was designed and the shelled charges model (SCM)/SRE with protective armor impacting by shaped charge tests were conducted. Air overpressures at 5 locations and axial acceleration caused by the explosion were measured, and the experimental results were compared with two air overpressure curves of propellant detonation obtained by related scholars. Afterwards, the finite element software AUTODYN was used to simulate the SCM impacted process and SRE detonation results. The penetration process and the formation cause of damage were analyzed. The detonation performance of TNT, reference propellant, and the propellant used in this experiment was compared. The axial acceleration caused by the explosion was also analyzed. By comprehensive comparison, the energy released by the detonation of this propellant is larger, and the HMX or Al particles contained in this propellant are more than the reference propellant, with a TNT equivalent of 1.168–1.196. Finally, advanced protection armor suggestions were proposed based on the theory of woven fabric rubber composite armor (WFRCA).     

Deconsolidation and combustion performance of thermally consolidated propellants deterred by multi-layers coating

Both heating and solvent-spray methods are used to consolidate the standard grains of double-base oblate sphere propellants plasticized with triethyleneglycol dinitrate (TEGDN) (TEGDN propellants) to high density propellants. The obtained consolidated propellants are deterred and coated with the slow burning multi-layer coating. The maximum compaction density of deterred and coated consolidated propellants can reach up to 1.39 g/cm³. Their mechanic, deconsolidation and combustion performances are tested by the materials test machine, interrupted burning set-up and closed vessel, respectively. The static compression strength of consolidated propellants deterred by multi-layer coating increases significantly to 18 MPa, indicating that they can be applied in most circumstances of charge service. And the samples are easy to deconsolidate in the interrupted burning test. Furthermore, the closed bomb burning curves of the samples indicate a two-stage combustion phenomenon under the condition of certain thickness of coated multi-layers. After the outer deterred multi-layer coating of consolidated samples is finished burning, the inner consolidated propellants continue to burn and breakup into aggregates and grains. The high burning progressivity can be carefully obtained by the smart control of deconsolidation process and duration of consolidated propellants. The preliminary results of consolidated propellants show that a rapid deconsolidation process at higher deconsolidation pressure is presented in the dynamic vivacity curves of closed bomb test. Higher density and higher macro progressivity of consolidated propellants can be obtained by the techniques in this paper.     

基于DIFHA算子的动态直觉模糊多属性群决策方法

动态决策问题是现实中的一类常见问题。在提出动态直觉模糊混合平均(D IFHA)算子的基础之上,提供一种动态直觉模糊多属性群决策方法。该方法能同时考虑决策过程的阶段性和属性值位置对决策结果的影响,并较好地处理决策过程中的定性指标。分析和算例证实该方法的可行性和实用性。     

INTELLIGENT DECISION ALGORITHM FOR FAULT DETECTION AND ITS APPLICATION

ＩＮＴＥＬＬＩＧＥＮＴＤＥＣＩＳＩＯＮＡＬＧＯＲＩＴＨＭＦＯＲＦＡＵＬＴＤＥＴＥＣＴＩＯＮＡＮＤＩＴＳＡＰＰＬＩＣＡＴＩＯＮＷｕＪｉａｎｊｕｎ;ＺｈａｎｇＹｕｌｉｎ;ＣｈｅｎＱｉｚｈｉ（ＤｅｐａｒｔｍｅｎｔｏｆＡｅｒｏｓｐａｃｅＴｅｃｈｎｏｌｏｇｙ,...     

状态—参数联合估计方法及其在液体火箭发动机健康监控中的应用

基于传统的扩展卡尔曼滤波器（ＥＫＦ）,本文提出了一种带次优渐消因子的ＥＫＦ用于非线性时变随机动态系统状态与参数的联合估计。应用于液体火箭发动机健康监控算法的仿真研究表明,本文所提出的联合估计器具有较好的收敛性、实时性和动态跟踪能力。此外,文中还讨论了联合估计器应用于实际系统的有关问题。     

液体推进剂液滴高压蒸发研究

本文改进了现有的液体推进剂液滴高压蒸发模型,提出了一个计算高压下液滴蒸发时环境介质气体在液滴中溶解的子模型,该模型中采用了改进的R-K气体状态方程。利用本模型对丙烷在氮气中的高压蒸发进行了计算。结果表明在高压下液滴蒸发时间随压力和环境温度的增加而减小,当压力超过某临界值时,液滴将达到超临界状态。高压下环境介质气体在液滴中的溶解是非常明显的,并且压力愈高溶解性愈大,因此在推进剂高压燃烧中必须考虑溶解性对于液滴蒸发的影响。     

基于混合编码曝光的匀加速运动模糊图像复原方法

针对运动模糊图像复原问题中点扩展函数难以准确获得和图像反卷积的病态性,提出了一种基于混合编码曝光相机的运动模糊复原框架.混合编码曝光相机由一个高速双目立体相机和一个高分辨率编码曝光相机构成.编码曝光相机在其曝光过程中由一个二进制编码控制其快门的开关状态.双目立体摄像机作为一个运动传感器在编码相机曝光的开始、中间和结束时...