未来航空电子信息技术发展需求分析

从多平台OODA的任务运行出发,分析了未来航空电子信息技术主要面向多平台信息的高效组织与管理,其发展趋势是充分利用人工智能技术,将战场数据转换为信息,将信息演进为知识,从而形成具有反馈机制的环路来引导多平台航空电子体系更快的获取信息.本文分别从多域多维信息的高效获取,多异构平台分布式信息处理,高效智能的信息组织,清晰准...     

Comparative study of the influence of natural convection on directional solidification of Al–3.5 wt% Ni and Al–7 wt% Si alloys

We present numerical simulations of thermosolutal convection for directional solidification of Al–3.5 wt% Ni and Al–7 wt% Si. Numerical results predict that fragmentation of dendrite arms resulting from dissolution could be favored in Al–7 wt% Si, but not in Al–3.5 wt% Ni. Corresponding experiments are in qualitative agreement with the numerical predictions. Distinguishing the two fragmentation mechanisms, namely dissolution and remelting, is critical during experiments on earth, when fluid flow is dominant.     

高精度碳纤维复合材料反射面型面精度仿真分析

为全尺寸反射面的实际成型提供理论依据,本文通过建模仿真重点分析了外蒙皮装配偏差、自重及成型和使用温度差对反射面工作面型面精度（R. M. S）的影响。结果表明,当外蒙皮装配偏移量在0.5mm内时,其反射面工作面理论R. M. S值的变化量为0.47μm;在成型放置状态下,反射面11 kg自重其工作面理论R. M. S值变化量为0.55μm;反射面夹层结构的成型和使用温度差110℃,反射面工作面的理论R. M. S值变化量为17.79μm。     

一种低轨星座高精度相位保持方法

针对大型低轨星座在轨运行的高精度构型保持问题,提出了一种基于极限环的高精度相位保持方法。首先,推导了实际轨道与参考轨道的平相位角偏差与半长轴偏差的关系；然后,建立了基于极限环的相位保持周期以及半长轴改变量计算方法；最后,基于推导的半长轴偏差与相位偏差的关系,提出了一种相位保持实施方法。考虑地球非球形和大气阻力的数值仿真表明：本文提出的相位保持方法能够在卫星定轨数据精度不高、数据采样间隔较大的情况下,实现低轨星座系统的高精度相位保持。     

Hardware-In-the-Loop Simulations of spacecraft attitude synchronization using the State-Dependent Riccati Equation technique

A nonlinear control technique pertaining to attitude synchronization problems is presented for formation flying spacecraft by utilizing the State-Dependent Riccati Equation (SDRE) technique. An attitude controller consisting of relative control and absolute control is designed using a reaction wheel assembly for regulator and tracking problems. To achieve effective relative control, the selective state-dependent connectivity is also adopted. The global asymptotic stability of the controller is confirmed using the Lyapunov theorem and is verified by Monte-Carlo simulations. An air-bearing-based Hardware-In-the-Loop Simulator (HILS) is also developed to validate the proposed control laws in real-time environments. The SDRE controller is discretized for implementation of a real-time processor in the HILS. The pointing errors are about 0.2° in the numerical simulations and about 1° in the HILS simulations, and experimental simulations confirm the effectiveness of the control algorithm for attitude synchronization in a spacecraft formation flying mission. Consequently, experiments using the HILS in a real-time environment can appropriately perform spacecraft attitude synchronization algorithms for formation flying spacecraft.     

深空探测光量子通信信道的主要参数

深空探测器距离地球路程遥远,保持探测器与地面站高效、实时的信息通信,将探测器采集的科学数据及时、完整地传输回地球,是亟待解决的问题。量子通信可以在确保信息安全、增大信息容量以及提高检测精度等方面突破经典通信的物理极限,研究量子通信在深空探测中的应用意义非常。通过对深空量子通信信道的研究与分析仿真,得到光束发射角、接收器口径、收发端距离等与可靠量子通信的关系,为深空量子通信的工程实现提供设计、仿真依据。     

Signatures of the Sudden Stratospheric Warming events of January–February 2008 in Seoul,S. Korea

The period January–February 2008 was characterized by four Sudden Stratospheric Warmings (SSWs) in the Northern Hemisphere, of which the last warming, at the end of February 2008, was a major warming. A significant decrease in mesospheric water vapour (H₂O) of more than 2 ppmv (∼40%) was observed by the ground-based microwave (GBMW) radiometer in Seoul, S. Korea [37.3°N, 126.3°E] during the major SSW. A comparison with ground-based mesospheric H₂O observations from the mid-latitude station in Bern [46.9°N, 7°E] revealed an anticorrelation in the mesospheric H₂O data during the major SSW. In addition, prior to the major warming, strong periodic fluctuations were recorded in the Aura MLS vertical temperature distribution between 15 and 0.05 hPa at Seoul. The mesospheric temperature oscillation was found to have a period of ∼10–14 days with a persistency of 3–4 cycles.     

Collapse of a spheroidal cavitation bubble near a solid wall

Dynamics of a gas bubble in a liquid near a solid wall is studied. The influence of the initial spheroidal disturbances of the bubble shape and the distance to the wall on the dynamics of the bubble–liquid system is analyzed. The pressure in the bubble is initially greater than that of the surrounding liquid. An algorithm based on the Euler scheme and the boundary element method is applied in the calculations.     

微小型螺旋桨滑流内舵面操纵特性实验研究

微小型垂直起降飞行器悬停时往往采用螺旋桨滑流内舵面偏转进行姿态控制,但容易出现操纵力矩不足的问题。本文针对这一问题对微小型静推力状态螺旋桨与带舵面机翼的组合体进行了系统性的实验。通过对实验数据分析,本文指出通过优选螺旋桨几何参数可以改善操纵特性,并得出带舵面机翼不同构型对操纵特性影响的一系列结论,为如何改善此类飞行器悬停时的操纵特性提供了设计参考。     

一种个性化标签云中的标签排序算法

社会化标签能够直接反映用户兴趣和商品特征,因而可用于个性化推荐系统中。使用标签进行推荐时,需要将其排序,而现有标签云中的标签排序都是按标签被标记次数或字典顺序进行降序排列的,这些排列方式未考虑用户个性化的需求和标签的时效性。提出了一种个性化标签云中的标签排序算法,通过用户自身的兴趣与挖掘出的用户潜在兴趣进行标签排序,从而构建个性化的标签云,并根据用户兴趣的变化定期对标签云进行更新,可以更好地发现电子商务网站中用户感兴趣的商品。实验对比结果表明,个性化标签云中的标签排序算法能够有效的提高商品推荐质量。