计算机数控系统中的干扰源及抗干扰技术

分析了数控系统自身和工作环境中存在的各种干扰因素,具有针对性的从硬件／软件。从设计到生产采用了一系列实用的抗干扰技术,从而提高了数控系统的抗干扰能力和可靠性．     

基于模糊推理的无人战斗机视距空战机动决策

针对视距1vs.1空战场景下无人战斗机（Unmanned combat aerial vehicle, UCAV）的自主机动决策,提出了一种基于模糊推理的空战机动决策方法。首先,从空战场景出发,建立了角度、距离、速度及高度4种优势因子;其次,利用模糊规则对空战态势进行评估,将代表空战态势的优势因子输入模糊推理机,自适应地调整优势函数中各因子的权重;同时,利用决策机动、序列机动和惯性机动相结合的方法建立敌机位置预测模型,作为机动决策的辅助手段,最后利用试探机动进行机动决策。仿真结果表明模糊推理模型能够实现UCAV自主机动决策能力,模型的优势在于将模糊的空战态势转化为优势函数中确定的权重因子,在策略上指导UCAV做出更有针对性的机动决策。     

基于热流体动力润滑分析的滑动轴承平衡位置和动力特性系数研究(英文)

建立了考虑润滑油粘热效应的滑动轴承热流体动力润滑分析模型,采用有限元法分析滑动轴承油膜压力和温度分布。对有限元方程关于扰动项求导直接得到油膜压力对于各扰动项的偏导数,并且通过油膜压力对于扰动项的偏导数构建油膜力Jacobi矩阵。采用Newton-Raphson方法确定给定静载下的轴承平衡位置,同时不需要额外的计算即可通过油膜力Jacobi矩阵获得滑动轴承动力特性系数。通过算例研究了轴承几何参数对滑动轴承动力系数的影响。分析结果表明,油膜温度对轴承刚度系数的影响大于阻尼系数;在轴承偏心率较小时,轴承承载力和刚度系数随转速的增加而增大;而在轴承偏心率较大时,轴承承载力和刚度系数随转速的增加而减小。     

Helio-geomagnetic influence in cardiological cases

The effects of the energetic phenomena of the Sun, flares and coronal mass ejections (CMEs) on the Earth’s ionosphere–magnetosphere, through the solar wind, are the sources of the geomagnetic disturbances and storms collectively known as Space Weather. The research on the influence of Space Weather on biological and physiological systems is open. In this work we study the Space Weather   impact on Acute Coronary Syndromes (ACS) distinguishing between ST-segment elevation acute coronary syndromes (STE–ACS) and non-ST-segment elevation acute coronary syndromes (NSTE–ACS) cases. We compare detailed patient records from the 2nd Cardiologic Department of the General Hospital of Nicaea (Piraeus, Greece) with characteristics of geomagnetic storms (_DST${\mathrm{D}}_{\mathit{ST}}$), solar wind speed and statistics of flares and CMEs which cover the entire solar cycle 23 (1997–2007). Our results indicate a relationship of ACS to helio-geomagnetic activity as the maximum of the ACS cases follows closely the maximum of the solar cycle. Furthermore, within very active periods, the ratio NSTE–ACS to STE–ACS, which is almost constant during periods of low to medium activity, changes favouring the NSTE–ACS. Most of the ACS cases exhibit a high degree of association with the recovery phase of the geomagnetic storms; a smaller, yet significant, part was found associated with periods of fast solar wind without a storm.     

基于多层PCB的基板射频信号传输性能研究

随着射频产品的小型化,特别是射频SIP(systems in package)产品的逐渐应用,基于多层PCB的基板射频组件等射频集成产品的应用越来越多,基板内射频信号传输性能的研究也越来越重要。通过对基于多层PCB的基板射频传输性能进行仿真测试,验证了DC-40GHz范围内射频基板传输性能,针对射频传输中极为关注的传输损耗问题,通过改进介质厚度或者铜箔材料实现基板射频传输损耗的优化,单位长度传输线射频传输损耗减小20%以上。同时针对星载等应用环境,通过深层充放电、总剂量试验,表明多层PCB的基板满足星载等航天应用。     

Societal imperatives and the need for space nuclear power and propulsion systems

The development and exploitation of nuclear power and propulsion represent certain didactic imperatives for human civilization. Among these are economic, epistemological, moral and commercial propositions. Developing space nuclear power and propulsion represents one future; the choice of not to pursue the course barring some breakthrough in physics represents a dramatically different future. The author argues that the time is now fortuitous for deployment and operation of nuclear propulsion and power, primarily nuclear electric propulsion, at significant levels, employing figures of merit that transcend simple cost models used to justify nuclear power sources in the past. The proposition is examined, in the light of US and UN restrictions, to ascertain how best to proceed. The author argues that viewpoints of certain vocal albeit uninformed public interest groups are typically self-serving and generally categorically incorrect; it can be asserted that these same groups do not truly represent the public interest at all. It is, therefore, necessary to present an even-handed assessment of both sides of the argument to determine the virtues and liabilities of embarking on such a developmental path. Given the imperatives mentioned, the author argues that nuclear power and propulsion for space systems is a societal necessity.     

Some practical strategies for reducing intermodulation in satellitecommunications

Various heuristic procedures for obtaining practical solutions to the general one-level carrier frequency assignment problem are described. The problem treated is general in the sense that it accommodates the case where L of the N slots may be explicitly designated as prohibited and unavailable for assignment. This problem occurs in satellite transmission with many small carriers accessing the same transponder where, due to multipath and TV interference from crosspolarized transponders of the same satellite and from copolarized transponders of the adjacent satellites, some portions of the bandwidth of the considered transponder cannot be used. To permit comparison with respect to the intermodulation advantage and central-processing-unit time required, the case without prohibited slots is considered. The sequential insertion procedure in which, starting with two carriers at the two end slots, one additional carrier at a time is optimally inserted into one of the unassigned slots is found best when the ratio between the available bandwidth and the total carrier bandwidth is greater than about 125%. All the heuristic procedures produced assignments whose intermodulation advantages are all greater than the bandwidth ratio     

Interstellar dust models

Interstellar dust models, previously constrained only from the extinction curve, have been radically changed with the arrival of IRAS observations of the dust infrared emission. An important component of interstellar dust is likely to be made of small particles that show a fluctuating temperature upon impinging single photons and which can produce large near and mid infrared excesses ubiquitously observed in the Galaxy and external galaxies. The analysis of COBE data should soon improve our understanding of dust infrared emissivity and particularly for big grains in the submillimeter domain. We will discuss the key observations (spectral features, broad-band colors, correlations with gas tracers…) which put the best constraints on any dust models and show that the next generation of IR/submm satellites (ISO, SIRTF…) should improve our knowledge of interstellar dust composition and the dust redistribution of the stellar energy inside galaxies.     

New progress on space solar telescope

The design of the Space Solar Telescope (phase B) has been completed. The telescope system has been manufactured (phase C) since the beginning of 1999, and it will be assembled by the end of 2000. In this paper, mainly the optical design, technique and manufacture will be described. The launch is planned for the summer of 2004.     

High resolution imaging of objects at Ka band

A coherent wideband millimeter wave (mmW) imaging radar which operates in two different imaging modes is briefly described. The principles of two-dimensional (2-D) high resolution imaging are introduced. The image reconstruction algorithm together with image enhancement techniques are discussed. Some experiments imaging on both scaled aircraft model and full-size large scale vehicle are presented