多核处理器P2020的访存实时性分析与优化

多核处理器以其高集成度、高性能功耗比的特点，获得了军事、电信、网络等领域的关注，但多个处理核心对共享资源的抢占带来的实时性问题阻碍了多核处理器在上述领域的应用。面向实时性的代表指标———访存时间，以P2020为研究对象，分析了其实时性的影响因素，采用可变步长的模型，对各种影响因素进行了定量的测试与分析，为多核处理器访存实时性的优化提供了参考。     

Simulation study on slant-to-vertical deviation in two dimensional TEC mapping over the ionosphere equatorial anomaly

With the rapid increase of GPS/GNSS receivers being deployed and operated in China, real-time GPS data from nearly a thousand sites are available at the National Center for Space Weather, China Meteorology Administration. However, it is challenging to generate a high-quality regional total electron content (TEC) map with the traditional two-dimensional (2-D) retrieval scheme because a large horizontal gradient has been reported over east–south Asia due to the northern equatorial ionization anomaly. We developed an Ionosphere Data Assimilation Analysis System (IDAAS), which is described in this study, using an International Reference Ionosphere (IRI) model as the background and applying a Kalman filter for updated observations. The IDAAS can reconstruct a three-dimensional ionosphere with the GPS slant TEC. The inverse slant TEC correlates well with observations both for GPS sites involved in the reconstruction and sites that are not involved. Based on the IDAAS, simulations were performed to investigate the deviation relative to the slant-to-vertical conversion (STV). The results indicate that the relative deviation induced by slant-to-vertical conversion may be significant in certain instances, and the deviation varies from 0% to 40% when the elevation decreases from 90° to 15°, while the relative IDAAS deviation is much smaller and varies from −5% to 15% without an elevation dependence. Compared with ‘true TEC’ map derived from the model, there is large difference in STV TEC map but no obvious discrepancy in IDAAS map. Generally, the IDAAS TEC map is much closer to the “true TEC” than is STV TEC map is.     

Boundary condition modelling and identification for cantilever-like structures using natural frequencies

The actual boundary conditions of cantilever-like structures might be non-ideally clamped in engineering practice, and they can also vary with time due to damage or aging. Precise modelling of boundary conditions, in which both the boundary stiffness and the boundary mass should be modelled correctly, might be one of the most significant aspects in dynamic analysis and testing for such structures. However, only the boundary stiffness was considered in the most existing methods. In this paper, a boundary condition modelling and identification method for cantilever-like structures is proposed to precisely model both the boundary stiffness and the boundary mass using sensitivity analysis of natural frequencies. The boundary conditions of a cantilever-like structure can be parameterized by constant mass, constant rotational inertia,constant translational stiffness, and constant rotational stiffness. The relationship between natural frequencies and boundary parameters is deduced according to the vibration equation for the lateral vibration of a non-uniform beam. Then, an iterative identification formulation is established using the sensitivity analysis of natural frequencies with respect to the boundary parameters. The regularization technique is also used to solve the potential ill-posed problem in the identification procedure.Numerical simulations and experiments are performed to validate the feasibility and accuracy of the proposed method. Results show that the proposed method can be utilized to precisely model the boundary parameters of a cantilever-like structure.     

The Magnetospheric Multiscale Magnetometers

The success of the Magnetospheric Multiscale mission depends on the accurate measurement of the magnetic field on all four spacecraft. To ensure this success, two independently designed and built fluxgate magnetometers were developed, avoiding single-point failures. The magnetometers were dubbed the digital fluxgate (DFG), which uses an ASIC implementation and was supplied by the Space Research Institute of the Austrian Academy of Sciences and the analogue magnetometer (AFG) with a more traditional circuit board design supplied by the University of California, Los Angeles. A stringent magnetic cleanliness program was executed under the supervision of the Johns Hopkins University’s Applied Physics Laboratory. To achieve mission objectives, the calibration determined on the ground will be refined in space to ensure all eight magnetometers are precisely inter-calibrated. Near real-time data plays a key role in the transmission of high-resolution observations stored on board so rapid processing of the low-resolution data is required. This article describes these instruments, the magnetic cleanliness program, and the instrument pre-launch calibrations, the planned in-flight calibration program, and the information flow that provides the data on the rapid time scale needed for mission success.     

基于仿真分析的压铆力预测模型

铆接是飞机结构机械连接的主要方式,压铆力作为影响铆接质量的重要因素,传统的计算方法通常是建立在体积不变的假设之上,且不考虑钉杆材料被压入钉孔部分的体积,导致模型误差较大。为此,依据仿真分析结果和铆钉材料的流动趋势,引入体积缩减系数来描述钉杆被压入钉孔部分的体积,建立压铆力预测模型,并与已有的试验数据进行对比,结果表明计算值与试验值的一致性较好,该模型可以用来预测铆接过程中压铆力的大小。     

一种PowerPC和FPGA结构的远程接口单元设计方法

远程接口单元（ RIU）已经是综合化模块化航空电子系统的重要组成部分。分析了分布式IMA架构下航空电子系统对远程接口的新需求,提出了一种基于PowerPC ＋FPGA结构的远程接口单元设计方法。通过设计方法不仅实现了单元综合多种I／O资源,还保证了单元具有一定的容错和可配置特性,并在远程接口关键技术方面取得了实质性的突破。     

轮胎参数对双轮式起落架刹车耦合振动影响研究

目前对飞机起落架低频刹车耦合振动问题的研究主要停留在考虑轮胎参数影响的起落架纵向单自由度振动特性分析，对于多自由度低频刹车耦合振动的特性研究不足。基于Simcenter 3D 动力学分析软件建立双轮支柱式起落架刚柔耦合整机滑跑刹车分析模型，研究轮胎竖向刚度和侧偏刚度对双轮支柱式起落架低频刹车纵向、横向和扭转的多自由度耦合振动的影响。结果表明：轮胎的竖向刚度对起落架横向和扭转方向上的振动影响较大，轮胎竖向刚度变化33%，横向和扭转方向上的振动变化5% 左右；轮胎的侧偏刚度对起落架低频刹车横向上的振动影响较大，轮胎侧偏刚度变化33%，横向上的振动变化15% 左右。     

Performance analysis of wavefront curvature methods for rangeestimation of a moving source

In numerous practical situations a large array of sensors is required, especially for improving the system ability to detect and track moving sources. However, the array performance is strongly affected by the lack of stationarity of the impinging signals. The use of a large array of sensors allow us to perform the source localization by using the wavefront curvature. The analysis of the range estimates based on the wavefront curvature have been thoroughly performed by various authors but, to our knowledge, is restricted to the case of fixed sources. The study of the effects of source motion for range estimation (Section III) and source detection (Section V) constitutes an important part of this work. This study reveals that the array performance can be far from the expected values, especially for large array. Therefore, the robustness of a direct processing of the whole sensor array is very questionable. The computational burden constitutes another serious drawback of this (direct) approach. The use of partitioned processings (Sections IV and VI) seems thus quite promising even if (and perhaps because) it is not optimal so as to fulfil the computation cost and robustness requirements. The performance of such processings for estimating the range of moving sources is presented     

GPS/GLONASS/GALILEO实时服务（RTS）产品性能评估分析

目前,不同机构提供的GNSS实时服务产品性能存在差异。为了全面揭示实时服务产品的性能，为系统服务和用户应用提供参考，统计了各实时服务产品的历元完整率及卫星数量，基于实时轨道和钟差恢复方法，比较分析了产品精度，并评估了产品定位性能。研究结果表明：正常情况下，实时服务产品的历元完整率较高，基本可保持在95%以上，所提供系统的卫星数量保持稳定且充足。对于GPS，各机构卫星实时轨道平均精度基本一致，约为3cm，实时钟差精度略有差别。对于其他GNSS，不同机构产品精度存在差别。利用实时服务产品进行GPS实时精密单点定位的平面精度优于10cm，高程精度优于20cm。相对于GPS单系统，多系统联合定位精度基本一致，但收敛速度明显提升。     

Mg—Li合金的均化制度研究

对Mg-Li合金的均匀化工艺及制度进行了研究。实验表明，铸锭包覆铝箔的方法可以使均化过程顺利进行；确定了Mg-Li二元合金的均化制度为300℃×24h，添加合金元素的Mg-7Li-14Zn三元以上的合金均化制度确定为300℃×36h。