测控资源调度管理系统的构造与实现

针对我国航天测控实际问题的特点和现状,基于知识发现提出了测控资源动态调度算法的框架,在此基础上,基于数据仓库建立了测控资源动态调度管理系统的体系结构,并采用面向对象(Ob ject-O riented,O-O)技术,分析和设计了测控资源动态调度管理系统,最后阐明了该系统的优点。实际应用表明,该方法使我国“一网管多星”的效率得到极大的提高。     

基于分级优化的飞机翼面结构布局综合技术研究

为了探讨飞机翼面结构主要纵横骨架的最佳布局问题．并提供符合工程实际的、用于概念设计阶段的飞机结构设计方法,本文采用分级优化与集成的策略,该策略分为三个层次。第一个层次为拓扑优化,并由此确定纵向骨架的个数与位置的最优布局;第二个层次为尺寸优化,它用来确定翼面的中间参数;第三个层次为稳定性准则优化,它确定横向骨架的个数与位置的最优布局。在分级优化的三个层次中,拓扑优化是独立的,尺寸优化与稳定性准则优化是相互耦合的。以国外某飞机机翼为例,结果表明本文提出分级优化的思路与所采用的集成方法是可行的,并且具有很好的数值效果。作者认为：它对从事飞机结构设计的人员有一定的指导性和参考价值,值得在飞机设计部门推广应用。最后,总结给出五点结论供参考。     

双脉冲固体火箭发动机隔塞运动特性

以双脉冲固体火箭发动机隔塞的运动过程为研究对象,搭建了脉冲隔离装置冷气冲击实验平台,获得了隔塞在Ⅰ脉冲燃烧室中的运动规律.采用动态结构嵌套网格方法,对隔塞的运动过程进行了数值模拟,分析了隔塞运动过程中流场结构,揭示了隔塞运动规律的形成机制.研究结果表明:对于单孔隔板,隔塞在燃烧室中沿轴向平稳运动,随着驱动压强的上升,隔...     

含多处损伤未加筋铝合金壁板的剩余强度

 进行了含多处损伤（MSD）的未加筋LY12CZ铝合金壁板的剩余强度试验。用0.12的钼丝切割预制裂纹,在垂直于裂纹面的方向施加单调增加的拉伸载荷,直至壁板破坏。得到了含不同裂纹几何的未加筋壁板的剩余强度。试验结果表明随着主裂纹长度增加,未加筋壁板的剩余强度减小;对相同的主裂纹长度,主裂纹和相邻的MSD裂纹之间的距离b减小,平板的剩余强度也减小。用5种失效准则分别计算了每个壁板的剩余强度。与试验结果的比较表明,净截面屈服准则和表观断裂韧性准则的误差较大,塑性区连通准则预测的平均误差为22.17%,改进的表观断裂韧性准则的平均误差为16.98%,而改进的塑性区连通准则预测的平均误差为8.27%,改进的塑性区连通准则大大提高了预测结果的精度。     

太阳系边际探测飞行任务规划

针对太阳系边际探测任务,开展了星际多目标飞越的任务规划,采用小推力混合优化设计方法完成了基于借力飞行及电推进技术的行星际转移轨道联合优化设计,对比研究了面向日球层鼻尖和尾部探测的星际多目标探测飞行方案。研究表明,探测器在2024-2025年发射,可飞抵日球层鼻尖区域,在2027-2030年发射可飞抵日球层尾部区域,并可在2049年1月1日前飞离日心100 AU,实现太阳系边际空间的科学探测。其中日球层鼻尖探测任务探测器飞抵100 AU的位置位于鼻尖中心区域,可与旅行者1号、2号探测器形成有效互补。文章所用任务规划方法,可为太阳系边际探测的自主任务规划技术提供基础,相关研究成果能够为未来中国首次太阳系边际探测任务的实施提供有价值的参考。     

航空发动机高压转子试验模型的动力学相似设计

为了获得能够替代航空发动机转子原型进行动力学试验的模型，提出了发动机转子系统试验模型的动力学相似设计方法。采用相似理论推导了转子系统缩比模型的动力学相似准则，继而建立缩比模型与原型的动力学相似关系。通过动力学优化方法对转子缩比模型的动力学等效模型进行修正，目标函数由固有频率、临界转速和振型组成。以双转子发动机高压转子系统的动力学相似设计为例，通过有限元仿真对设计方法的有效性进行了验证。结果表明，在设计转速范围内，动力学相似模型与原型的前两阶临界转速相似误差分别为3.92%和0.86%，对应振型的相关性均大于0.98，且模型与原型的模态应变能分布基本一致。通过该方法获得的动力学相似模型能够较好地预测原型的动力学特性，并有效降低模型试验的成本和难度。     

Introducing the law games: Predicting legal liability and fault in satellite operations

Over recent times there has been a rise in the number of objects placed into Earth orbit. With various countries licensing a number of large constellations, the orbital population is set to increase dramatically. A significant number of technical advances have facilitated this and, in the UK and elsewhere, this has been matched by the updating of legislation and an increased policy focus on the need for increased space surveillance and tracking. The rise of large constellations coupled with an increasing number of experimental techniques such as active debris removal or on-orbit servicing procedures means that establishing fault will be crucial if litigation is to be successful. In doing this, any legal proceedings will look at both norms of behaviour, deviation from which will point towards fault and the types and standard of evidence that will be required.This paper will outline these problems in detail. It will be proposed that what is required to map out the contours of liability are both codification of the norms for satellite operations and clarity on protocols for evidence gathering in cases where fault may be contested in orbital operations. This discussion will identify that a way in which this could be achieved is by the use of “space law games”. These are simulations, similar to military war games, in which fictional scenarios could highlight some of the key legal issues that might need to be dealt with. The paper will outline some of the ways in which the law games might work and pose questions as to what data and other considerations will be needed to make such simulations meaningful.     

基于PDCA循环的系统测试性设计方法

采用PDCA的核心思想，结合某型综合显示控制系统研发过程工程实际，提出了一套系统测试性设计的技术方法。通过将系统测试性设计过程按照“策划-实施-评估-改进”的戴明环循环思路，以测试性需求实现和验证为出发点，聚焦测试性设计技术状态风险管控，提出了测试性设计工作的关键技术路径，落实测试性设计过程闭环，可有效指导系统测试性设计。     

Catching spiral – S0 transition in groups. Insights from SPH simulations with chemo-photometric implementation

We are investigating the co-evolution of galaxies within groups combining multi-wavelength photometric and 2D kinematical observations. Here we focus on S0s showing star formation in ring/arm-like structures. We use smooth particle hydrodynamical simulations (SPH) with chemo-photometric implementation which provide dynamical and morphological information together with the spectral energy distribution (SED) at each evolutionary stage. As test cases, we simulate the evolution of two such S0s: NGC 1533 and NGC 3626.     

Galaxy evolution in groups. USGC U268 and USGC U376 in the Leo cloud

With the aim of investigating galaxy evolution in nearby galaxy groups, we analyzed the spectral energy distribution of 24 galaxies, members of two groups in the Leo cloud, USGC U268 and USGC U376. We estimated the ages and stellar masses of the galaxies by fitting their total apparent magnitudes from far-ultraviolet to near-infrared with population synthesis models. The comparison of the results for a subsample of galaxies with smooth particle hydrodynamic (SPH) simulations with chemo-photometric implementation, shows that in most cases the estimated stellar masses obtained with the two different approaches are in good agreement. The kinematical and dynamical analysis indicates that USGC U268 is in a pre-virial collapse phase while USGC U376 is likely in a more evolved phase towards virialization.