ATM局域网仿真技术

简要介绍了 Ａ Ｔ Ｍ 局域网仿真的主要原理，以 Ｉ Ｂ Ｍ ８２６０ Ａ Ｔ Ｍ 交换机为例，具体分析了 Ａ Ｔ Ｍ 局域网仿真的实现细节。     

一种改进的防空导弹侧向回路稳定控制结构分析

基于复合稳定控制结构,对某防空导弹侧向回路过载反馈通道的结构进行了改进。基于理论分析,结合工程应用实际进行了数学仿真验证。结果表明:在保持足够稳定裕度的前提下,改进结构的系统快速性好,鲁棒性更优。     

Crew autonomy for deep space exploration: Lessons from the Antarctic Search for Meteorites

Future piloted missions to explore asteroids, Mars, and other targets beyond the Moon will experience strict limitations on communication between vehicles in space and control centers on Earth. These limitations will require crews to operate with greater autonomy than any past space mission has demonstrated. The Antarctic Search for Meteorites (ANSMET) project, which regularly sends small teams of researchers to remote parts of the southern continent, resembles a space mission in many ways but does not rely upon a control center. It provides a useful crew autonomy model for planners of future deep space exploration missions. In contrast to current space missions, ANSMET gives the crew the authority to adjust competing work priorities, task assignments, and daily schedules; allows the crew to be the primary monitor of mission progress; demands greater crew accountability for operational errors; requires the crew to make the most of limited communication bandwidth; adopts systems designed for simple operation and failure recovery; and grants the crew a leading role in the selection and stowage of their equipment.     

一种源包和虚拟信道相结合的AOS调度算法

针对目前高级在轨系统(AOS)应用中遥测调度算法大多没有同时支持源包和虚拟信道2级调度的问题,提出一种基于AOS遥测源包调度和虚拟信道调度相结合的算法,实现同时对源包调度和虚拟信道调度层面的支持。针对源包调度,提出一种基于源包刷新率的动态优先级调度算法,以保证实时数据及时下传。针对虚拟信道调度,提出一种采用最重要(VIP)/同步/异步相结合的3级调度,保证信道的合理分配利用。分别采用源包调度策略、虚拟信道调度策略和文章提出的算法策略,对某航天器下行数据的平均时延进行仿真。仿真结果表明:文章提出算法策略的平均时延,低于源包调度策略和虚拟信道调度策略,比单独采用源包调度或者虚拟信道调度的算法具有更高的复用效率和公平性。     

卫星通信地面终端射频一致性测试及仿真分析

介绍了卫星通信系统体制、地面终端的基带处理过程,以及发射机射频指标和测试算法,利用MATLAB和ADS软件搭建了基带信号生成模块、发射机模块,对终端发射机的发射功率、误差矢量幅度、占用带宽、邻道干扰进行了仿真。仿真结果表明,上变频器的射频带宽过小会使调制信号的误差矢量幅度增大,放大器工作在非线性区会对占用带宽和邻道干扰有较大影响,使发射机不满足射频一致性要求。本文的研究结果对设计卫星通信地面终端具有一定的借鉴意义。     

高旋转数内冷通道换热实验技术及验证

通过内冷通道换热理论分析及实验系统优化,获得了使内冷通道内气体压力保持在500kPa以上的高旋转数实验技术.旋转数和雷诺数的范围分别为0~2.08,104~7×104,极大满足了旋转数与雷诺数同时覆盖真实发动机涡轮叶片工作参数的实验需求.证实了雷诺数和旋转数对内冷通道换热的影响可以解耦.而应用该实验技术进行同等旋转数实验时,内冷通道热损失占总加热量的比例和实验误差分别降低到18%和±10%.     

综合模块化航空电子系统远程加载技术研究及性能分析

随着飞机航空电子系统综合化程度的提高，软件的部署、加载和更新的复杂度也在逐步提高。传统软件更新后，需要在地面为每个模块进行升级，并将新版本的软件映像文件固化在模块上，这种更新周期长且流程复杂。随着通用模块和应用重构的发展，软件映像需要部署在系统的各个冗余备份节点中，从而使其更新的流程更为复杂。本文针对以上问题提出了基于光纤通道和 ARINC653操作系统的远程数据加载系统，以使系统在上电、重启及重构时可实现从大容量存储模块上远程加载操作系统内核映像、分区应用及自启动功能。在功能实现的基础上，本文对远程加载和本地加载的时间性能进行了分析和比较。     

Capillary flow rate limitation in asymmetry open channel

This paper focuses on the stability of capillary forced flow.In space,open capillary channels are widely used as the liquid and gas separation devices to manage liquid positioning and transportation.Surface collapse happens when the flow rate exceeds the critical value,leading to a failure of propellant management.Knowledge of flow rate limitation is of great significance in design and optimization of propellant management devices(PMDs).However,the capillary flow rate limitation in an asymmetry channel has not been studied yet in the literature.In this paper,by introducing an equivalent angle to convert the asymmetry corner to a symmetry one,the one-dimensional theoretical model is developed.The flow rate limitation can then be investigated as a function of the channel geometry as well as liquid property based on the model.Comparisons between the asymmetry and symmetry channels bring forth the characteristics of the two kinds of channels,and demonstrate good accordance between the new advanced model and the existing one in the literature.This theoretical model can provide valuable reference for PMD designers.     

复合铣整体叶盘通道加工工艺规划分析

首先对开式整体叶盘通道几何特征进行分析,在宽度和深度上对通道加工空间进行计算,从轴向和径向进行切削加工性分析;通过偏置面求解及其延伸面求解,进而确定可加工区域;在对比分析各种铣削方法基础上,优选复合铣削数控刀具,明确通道复合铣加工方法以及流程,为后续开式整体叶盘通道加工工艺优化打下基础。     

基于仲裁环的光纤通道性能分析

随着航空电子系统的发展，光纤通道技术正在逐渐取代传统的总线型通信网络。仲裁环作为一种经济的光纤通道拓扑结构，目前得到了较广泛的研究。本文利用OPNET modeler建立了光纤通道仲裁环及其节点状态机模型，并通过仿真对基于仲裁环的光纤通道性能进行了分析，为深入研究光纤通道奠定了理论基础。