Energetic particle signatures of geoeffective coronal mass ejections

We have studied statistically associations of moderate and intense geomagnetic storms with coronal mass ejections (CMEs) and energetic particle events. The goal was to identify specific energetic particle signatures, which could be used to improve the predictions of the geoeffectiveness of full and partial halo CMEs. Protons in the range 1–110 MeV from the ERNE experiment onboard SOHO are used in the analysis. The study covers the time period from August 1996 to July 2000. We demonstrate the feasibility of energetic particle observations as an additional source of information in evaluating the geoeffectiveness of full and partial halo CMEs. Based on the observed onset times of solar energetic particle (SEP) events and energetic storm particle (ESP) events, we derive a proxy for the transit times of shocks driven by the interplanetary counterparts of coronal mass ejections from the Sun to the Earth. For a limited number of geomagnetic storms which can be associated to both SEP and ESP signatures, we found that this transit time correlates with the strength of geomagnetic storms.     

空中交通管制仿真环境研究

研究可支持训练和多种用途的空中交通管制(ATC)仿真方法,介绍了空中交通管制的仿真内容,通过分析空中交通管制的各要素,建立了仿真环境框架和仿真环境模型.采用分布交互仿真技术和虚拟现实技术,讨论了仿真环境中视景数据库的生成、三维视景实时生成、管制设备仿真、计算机生成飞机、想定生成和任务管理等问题,最后介绍了系统的实现结果.     

Stewart平台远程操作试验系统的研制

为了研究Stewart平台大时延情况下的远程操作稳定性,建立了相关试验系统.用以太网模拟远程通信信道,连接2套Stewart平台控制系统;利用DirectX技术,对用户屏蔽了具体硬件设备,建立了用户输入接口和视频反馈;利用OpenGL(Open Graphic Library)技术,建立了虚拟操作环境,以便于未来利用虚拟操作环境补偿时延;用神经网络的位置正解方法代替传统方法驱动虚拟模型,获得更高的精度;对通讯的带宽进行在线监控,优先保证指令传输;通过改变发送速率,保证视频连续发送.试验结果表明,用户通过输入指令可以方便地控制平台,平台位姿可以通过虚拟操作环境和视频进行反馈,系统满足了设计要求.      

Solar proton enhancements in different energy channels and coronal mass ejections during the last solar cycle

The main properties of 11622 coronal mass ejections (CMEs) observed by the Solar and Heliospheric Observatory (SOHO) mission’s Large Angle and Spectrometric Coronagraph (LASCO-C2) from January 1996 through December 2006 are considered. Moreover, the extended database of solar proton enhancements (SPEs) with proton flux >0.1 pfu at energy >10 MeV measured at the Earth’s orbit is also studied. A comparison of these databases gives new results concerning the sources and acceleration mechanisms of solar energetic particles. Specifically, coronal mass ejections with width >180° (wide) and linear speed >800 km/s (fast) seem they have the best correlation with solar proton enhancements. The study of some specific solar parameters, such as soft X-ray flares, sunspot numbers, solar flare index etc. has showed that the soft X-ray flares with importance >M5 may provide a reasonable proxy index for the SPE production rate. From this work, it is outlined that the good relation of the fast and wide coronal mass ejections to proton enhancements seems to lead to a similar conclusion. In spite of the fact that in the case of CMEs the statistics cover only the last solar cycle, while the measurements of SXR flares are extended over three solar cycles, it is obvious for the studied period that the coronal mass ejections can also provide a good index for the solar proton production.     

Interplanetary coronal mass ejections during the descending cycle 23: Sheath and ejecta properties comparison

We have used Omniweb data in order to identify the sheath and the ejecta boundaries of 67 shock-driving interplanetary coronal mass ejections during the time period 2003–2006. We examine and compare their statistical properties (speed, magnetic field strength, proton density and temperature, proton plasma beta), with those of the typical solar wind. We also calculate their passage time and radial width. We study the correlation between the ejecta and sheath characteristics.     

深空探测器在轨推力器参数辨识方法

针对中国首次自主火星探测任务需要,结合环绕器质量特性和推进系统布局构型,分析了喷气卸载对整器角动量的影响。在分析的基础上,通过飞轮卸载前后三轴转速变化规律,计算整器角动量变化情况,并解算出每次喷气时产生的冲量及推力方向偏差;通过同组推力器作用时对各轴的扰动,解算整器质心坐标。利用在轨数据分析了天问一号探测器巡航段6次使用不同推力器的喷气卸载情况,解算的推力器方向偏差、质心坐标和地面设计值进行比对,实测推力方向偏差不超过0.6°,质心绝对偏差小于18mm,验证了计算方法的有效性和正确性,可作为后续轨控任务的点火方向制定、燃料预算的输入依据。     

射流预冷对涡扇发动机控制计划的影响及验证

射流预冷(MIPCC)会导致发动机共同工作线会发生改变,进而影响发动机的工作特性.通过分析射流预冷对双转子涡扇发动机部件和整机的影响,特别是射流预冷对高低压转子转差的影响,掌握了射流预冷对控制计划的影响特性,在此基础上完善了相关控制计划,并通过试验验证了控制计划的有效性,结果表明:发动机低压转子转速控制静差由2.6％减...     

变外涵工况下风扇增压级双涵匹配机理

针对某型民机大涵道比风扇增压级,在不同外涵工况下开展数值计算,旨在研究风扇增压级双涵性能匹配规律和相应机理。通过分析计算结果,掌握了外涵工况对内涵特性的影响规律:当外涵工况从近堵点移向近喘点的过程中,内涵的流量、总压比、效率逐渐增大,且内涵稳定裕度呈持续增大的变化规律。同时也在获取内涵特性时,掌握了外涵气动性能的变化规律,在不同外涵工况下阐明了内涵逼喘过程中双涵气动性能的相互匹配机理取决于风扇的总压比?流量特性和内外涵流量再分配机制的共同作用。      

基于蒙特卡罗法的航空发动机稳态空气系统网络计算

为了解决目前稳态空气系统算法在求解复杂网络时不容易获得收敛解的问题,将航空发动机稳态空气系统简化为由节点和元件组成的网络,借助概率思想计算连续性方程和能量方程,建立相应的随机游动模型,运用蒙特卡罗方法求解各节点的压力,再根据流量与元件两端压力的关系,计算流经各元件的流体流量。将计算得到的不同工况下航空发动机稳态空气系统内部节点的压力和流量值,与flowmaster计算结果进行比较,二者吻合较好,压力最大偏差为0.628%。蒙特卡罗方法与网络法相比,优势在于计算简便,且不会出现无法求解复杂空气系统网络的情况。     

基于SCORM标准的航空发动机虚拟、仿真研究

以航空发动机实验课程为例,采用SCORM标准和VRML技术建立了3D航空发动机虚拟仿真实验室,并在Blackboard平台上成功运行。其中详细介绍了3D图形轻量化方法和SCORM数据包的制作。实践证明,该虚拟实验室能实现3D演示、且具有较强的交互性,为学习者提供了良好的教学体验。