Effect of the Interplanetary Electric Field on the Magnetopause From Global MHD Simulations

The north-south component B_z of the Interplanetary Magnetic Field (IMF) and solar wind dynamic pressure P_d are generally treated as the two main factors in the solar wind that determine the geometry of the magnetosphere. By using the 3D global MHD simulations, we investigate the effect of the Interplanetary Electric Field (IEF) on the size and shape of magnetopause quantitatively. Our numerical experiments confirm that the geometry of the magnetopause are mainly determined by P_dB_z, as expected. However, the dawn-dusk IEFs have great impact on the magnetopause erosion because of the magnetic reconnection, thus affecting the size and shape of the magnetopause. Higher solar wind speed with the same B_z will lead to bigger dawn-dusk IEFs, which means the higher reconnection rate, and then results in more magnetic flux removal from the dayside. Consequently, the dayside magnetopause moves inward and flank magnetopause moves outward.      

Dust Acoustic Wave in Dusty Plasmas With Streaming Ions Under Ultraviolet Irradiation

The reductive perturbation method is applied to investigate the dust acoustic soliton in dusty plasmas with streaming ions under ultraviolet irradiation theoretically and numerically. The self-consistent dust charge variation is taken into account. It is shown that the ultraviolet irradiation can significantly lower the magnitude of the dust negative charge, and ion streaming velocity firstly raise the magnitude of the dust negative charge and then lower it. With the growth of (Ultraviolet) UV photo flux or ion streaming velocity, the phase velocity and width of the solitary waves decrease, whereas its amplitude increases.      

极端太阳风条件下的磁层顶位形

基于极端太阳风条件下的三维MHD数值模拟数据, 构建了一种极端太阳风条件下的三维非对称磁层顶位形模型. 所提出的模型考虑了行星际南向磁场(IMF) B_z日下点距离侵蚀的饱和效应, 太阳风动压B_d对磁层顶张角影响的饱和效应, 赤道面、昼夜子午面磁层顶的不对称性以及极尖区的内凹结构和内凹中心的移动, 并利用Levenberg-Marquart多参量非线性拟合方法拟合了模型参数. 数值模拟研究表明, 在极端太阳风条件下, 随B_d增大, 磁层顶日下点距离减小, 磁层顶磁尾张角几乎不变; 随南向(IMF)B_z增大, 磁层顶日下点距离略有减小, 磁层顶磁尾张角减小, 极尖区内凹中心向低纬移动. 通过对2010年8月1日太阳风暴事件验证发现, 本文所建立的模型能够描述极端太阳风条件下的三维磁层顶位形.      

Research Progress of Solar Corona and Interplanetary Physics in China: 2010-2012

The scientific objective of solar corona and interplanetary research is the understanding of the various phenomena related to solar activities and their effects on the space environments of the Earth. Great progress has been made in the study of solar corona and interplanetary physics by the Chinese space physics community during the past years. This paper will give a brief report about the latest progress of the corona and interplanetary research in China during the years of 2010?2012. The paper can be divided into the following parts: solar corona and solar wind, CMEICME, magnetic reconnection, energetic particles, space plasma, space weather numerical modeling by 3D SIP-CESE MHD model, space weather prediction methods, and proposed missions. They constitute the abundant content of study for the complicated phenomena that originate from the solar corona, propagate in interplanetary space, and produce geomagnetic disturbances. All these progresses are acquired by the Chinese space physicists, either independently or through international collaborations.      

基于实验的自适应随机测试效率分析

自适应随机测试通过自适应算法对随机测试进行加强,从而提高软件失效检测能力.现有研究过多强调了其在F-度量上的优势,而较少考虑输入域的诸多因素对自适应随机测试效率的影响.选取3类典型自适应随机测试算法和随机测试算法,分析被测软件失效区域紧致程度、维度对算法的影响,并选取自适应随机算法中测试效果最佳的固定候选集算法在非数值条件下与随机算法比对.结果表明,自适应随机测试受输入域的诸多因素影响,适用性有限,实际测试中对测试效率的提升效果并不明显.      

多孔介质表面预混火焰熄火特性实验

对微型燃烧室中多孔介质表面预混火焰开展了不同孔径、孔隙率的多孔介质出口流场特性和熄火特性实验研究.研究结果表明:相对于圆管流,多孔介质出口流场边界层变薄,主流区宽度增加约50%,速度波动最大可达到前者的2.2倍.多孔介质孔径相同时,随孔隙率减小,或孔隙率相同时,随孔径减小,主流区的速度波动幅值均减小,在小孔径下更为明显,最大速度波动幅值从2.435m/s减小至1.099m/s.多孔介质表面预混火焰的熄火特性受出口流场和火焰形态的影响很大,孔隙率减小或孔径减小都会使相同当量比下熄火速度增加,多孔介质参数的影响最大可使熄火速度增加近1倍.      

基于可达集方法的结冰飞机着陆阶段安全风险评估

飞机在着陆过程中极易发生结冰的现象,结冰对飞行安全造成的危害极为严重。结冰导致飞机发生危险的原因是由于机翼或尾翼被冰层覆盖后空气动力学行为发生改变,飞机受力异常难以控制。为分析结冰后飞机的稳定性以保证飞行安全,以飞机纵向动力学系统为分析对象,将飞机结冰后状态的描述以可达集的形式进行,直观地判断飞机状态是否可控,以此确定飞机是否处于安全状态。以求解所得的可达集为基础,利用极值定理分析结冰飞机的风险概率模型,由模型计算不同情况下飞机的风险概率,最终得到飞机着陆阶段的安全风险评估结果,并由评估结果指导驾驶员操纵,从而保证飞机的安全飞行。     

QAR超限事件飞行操作风险诊断方法

利用某机型的快速存取记录器(QAR,Quick Access Record)数据,对飞机着陆阶段出现的某一QAR超限事件,选取飞机下降率、俯仰角等飞行员综合操作指标在无线电高度20 feet(1 feet=0.304 8 m)的数值以及20~0 feet之间的变化率,分析由这些指标构成的"空间"中发生该QAR超限事件的"高风险子空间".对同一机场同一机型的多个航班数据初步分析得到,着陆总重大于62 t、着陆温度小于32℃时,正常样本与QAR超限样本占比接近,表明环境因素并非该样本空间中QAR超限事件的主要因素.为进一步诊断,以超限事件发生率最大化为目标,以划分空间中包含的样本满足一定数量标准为约束,建立数学模型,并以黄金分割法为基础设计了算法,找出这些操作指标上区间的边界值,以此诊断可能触发该QAR超限事件的高风险区域,为飞行员模拟机针对性训练提供指导.      

基于域对抗门控网络的变工况刀具磨损精确预测方法

刀具磨损的精确预测对保证零件加工质量、提高生产效率和降低制造成本具有重要作用。在实际加工过程中,切削参数、刀具几何参数、刀具材料等工况复杂多变,工况信息和刀具磨损量对监测信号的耦合作用为刀具磨损的精确预测带来了很大挑战。针对以上问题,提出了一种基于域对抗门控网络（DAGNN）的变工况刀具磨损精确预测方法。引入工况分类网络并利用无磨损量标签样本,通过域对抗和门控过滤机制自适应地从不同工况的原始监测信号中提取表征刀具磨损且对工况变化不敏感的关键信号特征。对信号特征提取网络和刀具磨损预测网络进行迭代优化,从而实现变工况刀具磨损的精确预测。实验结果表明：相比已有的方法,本文方法能够利用少量带磨损量标签的目标工况样本实现刀具材料和刀具直径变化情况下的刀具磨损量精确预测,预测精度大幅提高。