新一代中频检前记录器设计与实现

由于中频检前信号包含丰富的信息,对于事后数据分析具有重要意义,目前,国内对中频检前记录器的需求呈上升趋势。新一代中频检前记录器不仅仅是作为实时解调器发生故障时的一种备份手段,而且成为了一种重要的数据获取手段。介绍704所研制的新一代中频检前记录器的设计思路与实现方法。     

信息系统灾难恢复的研究与实践

企业信息系统的灾难恢复是一项投资大、技术复杂的工程,需要在一套行之有效的方法论的指导下进行。通过对灾难恢复的原理分析,提出了以客户为中心的三角形体系框架。使用最优化理论对灾难恢复的策略进行了研究并在实际中得到应用。     

基于时间延迟理论的航空发动机维修优化模型

在对航空发动机维修现状进行分析的基础上,阐述了包括缺陷和故障两个因素的时间延迟模型的概念及其原理,并在系统分析航空发动机故障特点和维护特点的基础上,建立了航空发动机维修优化模型.通过对航空发动机维修周期模型进行实例研究,验证表明,时间延迟模型能够明显优化发动机的维修周期,提高航空发动机维修效能.     

实时离散事件系统的状态反馈逻辑

 基于状态时间的概念,在Ramadge-Wonham模型的基础上提出了一种新的实时离散事件系统模型。在控制目标是保持某给定谓词在闭环系统状态轨迹上为真的情况下,给出了实时控制不变性的定义。研究表明,对这类系统,存在一个状态反馈控制器使给定谓词在闭环系统状态轨迹上保持为真的充要条件是该谓词是实时控制不变的。证明了给定谓词所含的最大实时控制不变子谓词的存在性并给出了计算方法。最后,给出一个例子来说明有关结果。     

无人机机载导弹落角和时间控制导引律研究

改进了一种能同时控制命中角和命中时间的修正比例导引律,将其用到无人机机载空对地导弹中,将其中的剩余时间估计加入了命中角约束的影响,旨在保证无人机机载导弹垂直命中目标的同时,使命中时间更为准确.通过对此导引律和一种仅考虑垂直命中角约束的修正比例导引律以及和改进前导引律的比较,仿真表明,此导引律使无人机机载导弹能在保证垂直...     

Contributing Factors to Temporal and Spatial Associations in Mental Representations of Maps

Abstract

The present work explores an interactive model of spatial and temporal information in map memory. In four experiments, participants learned a map with temporal and spatial information confounded or unconfounded. Attentional and representational levels of information were made apparent through tasks that tap spatial, temporal, or other information. Learning criteria emphasizing sequential order or location imposed differential weighting of the information types in memory. Results indicate that map memory is spatial, but also interacts with the order in which map locations are encountered. Findings show flexibility in allocating attention and information indexing of location and sequential order information in map learning.     

电站典型大滞后过程自适应预估控制器设计及应用

电站典型大滞后过程难于控制的原因在于其大滞后本身导致系统不稳定及锅炉负荷频繁变化导致的参数时变特性。本文设计了一种模型参考自适应预估控制算法,引入二阶惯性与时间滞后两个补偿器,其主要参数如增益、时间常数和滞后时间均可在线自适应调整,致使过程与参考模型时刻匹配。该算法已应用于电站200 MW锅炉机组再热汽温过程控制,控制精度达到2℃以内。     

Time step size and model stiffness in the simulated slew of a tow of square sails

In order to assess space tow solar sail stability and control feasibility, slew simulations are performed for a simplified but dynamically representative km-class tow-like sail of sixteen 25 m square units (10,000 m² total area and 110 kg gross mass) with a 250 kg payload. It is seen that, for the dimensions considered, the space tow concept is structurally sound and its control is feasible. While observed instabilities are identified as numeric in nature and are eliminated accordingly, their very occurrence highlights the need for a refinement of the model for future studies. The analyses are carried out with custom software implementing non-standard implicit-iterative time integration with innovative elements. A new damping model, specifically tailored for the analysis of truly gossamer systems such as solar sails, is also proposed.     

Real-time global MHD simulation of the solar wind interaction with the earth’s magnetosphere

We have developed a real-time global MHD (magnetohydrodynamics) simulation of the solar wind interaction with the earth’s magnetosphere. By adopting the real-time solar wind parameters and interplanetary magnetic field (IMF) observed routinely by the ACE (Advanced Composition Explorer) spacecraft, responses of the magnetosphere are calculated with MHD code. The simulation is carried out routinely on the super computer system at National Institute of Information and Communications Technology (NICT), Japan. The visualized images of the magnetic field lines around the earth, pressure distribution on the meridian plane, and the conductivity of the polar ionosphere, can be referred to on the web site (http://www2.nict.go.jp/y/y223/simulation/realtime/).The results show that various magnetospheric activities are almost reproduced qualitatively. They also give us information how geomagnetic disturbances develop in the magnetosphere in relation with the ionosphere. From the viewpoint of space weather, the real-time simulation helps us to understand the whole image in the current condition of the magnetosphere. To evaluate the simulation results, we compare the AE indices derived from the simulation and observations. The simulation and observation agree well for quiet days and isolated substorm cases in general.     

通道间延迟时间差评价结果的不确定度

介绍了四参数正弦波最小二乘法评价通道间延迟时间差指标及不确定度分析和评价过程，同时给出了一个分析评价实例。该过程及结论可应用在对于测量标准进行相应指标的不确定度分析上，也可用于估计指标本身的不确定度。