航天器运输包装箱仿真验证平台技术研究

针对数量有限的物理跑车试验无法满足减振与保温性能测试需求的问题，提出一套航天器运输包装箱动力学与热学仿真验证方法，包括：建立适用于包装箱系统的刚柔耦合多体动力学系统，通过结合线路条件测试生成的动力学系统外部激励，实现减振性能虚拟跑车测试；建立基于计算流体力学的包装箱热学模型，通过模拟自然对流和空调控制，实现包装箱保温性能虚拟跑车测试；基于C/S架构和导航式流程设计思想，建立航天器运输包装箱仿真验证平台，通过实际案例证明该平台仿真结果与实际跑车测试数据具有较高的一致性。     

Study of highly perturbed spacecraft formation dynamics via approximation

This paper explores methods for approximating and analyzing the dynamics of highly perturbed spacecraft formations with an emphasis on computationally efficient approaches. This facilitates on-board computation or rapid preliminary mission design analysis. Perturbed formation dynamics are often approximated as linear time-varying (LTV) systems, for which Floquet theory can be used to analyze the degree of system instability. Furthermore, the angular momentum of the relative orbital state can be computed with the approximate dynamics to provide additional insight. A general methodology is developed first and then applied to the problem of unstable formation dynamics in asteroid orbits. Here the dominant perturbative effects due to low-order gravitational harmonics and solar radiation pressure are modeled. Numerical simulations validate the approach and illustrate the approximation accuracy achieved.     

Estimating the spin axis orientation of the Echostar-2 box-wing geosynchronous satellite

For the first time, the spin axis orientation of an inactive box-wing geosynchronous satellite has been estimated from ground-based optical photometric observations of Echostar-2’s specular reflections. Recent photometric light curves obtained of Echostar-2 over four years suggest that unusually bright and brief specular reflections were occurring twice within an observed spin period. These bright and brief specular reflections suggested two satellite surfaces with surface normals separated by approximately 180°. The geometry between the satellite, the Sun, and the observing location at the time of each of the brightest observed reflections, was used to estimate Echostar-2’s equatorial spin axis orientation coordinates. When considering prograde and retrograde rotation, Echostar-2’s spin axis orientation was estimated to have been located within 30° of either equatorial coordinate pole. Echostar-2’s spin axis was observed to have moved approximately 180° in right ascension, within a time span of six months, suggesting a roughly one year spin axis precession period about the satellite’s angular momentum vector.     

高温存储对Sn-Pb-Ni凸点界面金属间化合物生长的影响

倒装焊工艺由于具有信号处理速度快、封装密度高、可靠性高等特点，已广泛应用于高密度集成电路封装工艺中。高可靠倒装焊器件的互连焊点通常采用10Sn90Pb等高铅焊料，该焊料具有剪切强度高、可靠性高等优点，但其熔点高、回流工艺窗口窄等特性给封装工艺带来一定难度，此外该焊料在高温存储环境的可靠性有待进一步提高。本文采用Ni元素对10Sn90Pb焊料进行改性，研究高温存储下Sn-Pb-Ni体系凸点的力学性能以及金属间化合物（Intermetallic compound,IMC）的生长演变规律，以此评估Ni元素对10Sn90Pb凸点可靠性的影响。主要结果如下：适量添加Ni元素可以细化10Sn90Pb焊点界面处IMC晶粒，降低高温存储条件下的IMC生长速度，但在一定程度上会降低凸点的剪切强度。0.05%~0.1%含量的Ni元素添加对10Sn90Pb凸点综合性能提升较为显著。     

多臂协调操作自由飞行空间机器人的位置和内力混合控制

基于多臂自由飞行空间机器人多臂协调操使负载沿着期望的轨迹运动并且控制负载所受的内力为目的，在多臂自由飞行空间机器人系统协调操作的动力学方程基础上，推导了各个机械臂协调操作负载按期望轨迹运动时各个机械臂关节的驱动力矩的计算方法；给出了作用在负载的内力的定义，根据关节力矩计算方法和PID反馈控制原理，建立了多臂自由飞行空间机器人协调操作负载时的位置和内力的控制算法；讨论了所提出的控制算法的稳定性问题，得到了负载的位置误差和内力误差的约束条件。通过仿真实验证明该控制算法能够使负载的实际位姿和内力收敛到期望的轨迹和内力。     

用亚稳态正电子素研究络合的瞬态反应（Ⅲ）

本文用自制的装有 BaF_2探头的高探测效率的正电子湮没寿命谱仪测量了在室温下正电子素 o-Ps 与 p-RPhG 及 m-RPhG(R=NO_2,Cl,H,CH_3,cH_3O)在20%(V/V)二氧六环水溶液中的络合形成速度常数。实验结果表明,这些o-Ps-M 络合形成速度常数 K 值均与作为配位体的 p-RPhG、m-RPhG 的碱性解离常数 K 的负对数 pK_2 呈线性函数。这表明上述瞬态络合反应满足线性自由能关系,由此可推断出上述络合反应的一些重要性质。     

一种可伸缩空间机械臂及其应用分析

介绍一种能够完成多关节型空间机械臂所能承担的大部分空间任务 ,而且应用更简便的可伸缩空间机械臂 ,对其空间应用做出了一些设想 ,简单讨论了其应用的一些相关问题 ,肯定了其可行性和实用性。     

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with primary goat embryonic fibroblast showed no difference from traditional feederlayer-based culture method used in mouse and human. The putative primary EG colonies were multilayer clumps ofcompact cel     

密集编队气动耦合效应分析

简要介绍密集编队飞行时长机旋涡对僚机产生的气动耦合效应，以比奥特－萨瓦尔特定律为基础，初步分析由上洗及侧洗引起的升力、阻力和侧力变化，导出了编队稳定性导数的计算公式，计算及应用举例表明：模型化编队飞行时的气动耦合效应是有实际应用价值的。