带有参考信号的直接序列扩频系统

扩频通信系统中码同步的精度及其电路的复杂程度直接影响系统的性能、体积和成本。采用发射参考信号法可以简化接收机端的码同步电路 ,从而大大减小遥控遥测系统及无线局域网中扩频接收机的体积和成本。本文给出了采用 MAXIM芯片组实现 UHF频段带有发射参考信号的直接序列扩频系统 ,并通过 System View软件进行了仿真 ,结果表明该方法可获得较好的通信性能 ,易于工程实现     

Zadeh模糊推理算法的直觉化扩展

对Zadeh模糊推理算法进行了直觉化扩展.将Zadeh定义的模糊关系Rm进行直觉化扩展,推出了其对应的直觉模糊取式推理算法和直觉模糊拒式推理算法.以具体算例叙述了推理计算过程中的细节,验证了方法的正确性和有效性,并依据直觉准则,对其性能进行了评价.     

基于模糊理论的跳跃轨迹多目标优化设计

针对探月返回跳跃轨迹的多目标优化设计问题,提出了一种基于模糊理论的优化设计方法,并对非线性隶属度函数对优化结果的影响进行了研究.首先,将连续的无限维优化问题进行离散化,转化为非线性规划问题;其次,用隶属度函数将各个子目标进行模糊化,将多目标优化问题转化为求模糊判决隶属度函数的最大值问题;最后,求解经过模糊化的非线性规划问题.分析了探月返回跳跃轨迹的特性,表明模糊多目标优化更能体现决策者的偏好.构造了具有不同凹凸性、不同形状的非线性隶属度函数,比较了它们对优化结果的影响,结果表明隶属度函数影响多目标模糊优化结果的首要因素是隶属度函数的凹凸性.     

基于模糊层次分析法的机场管制模拟机评价

采用模糊综合评判法与层次分析法相结合的评估方法,对机场管制模拟机仿真度进行评价.根据机场管制模拟机需求功能选取恰当的评估指标,用层次分析法建立机场管制模拟机仿真度评价指标体系.然后分层次进行模糊综合评判,得出综合评价结果.最后以某机场管制模拟机为例,对其仿真度进行评估.结果表明这种方法科学合理且容易实现,为实验室设备选型提供了合理的依据,具有实际的应用价值.     

（20～400）MeV准单能中子参考辐射场的建立方法CSCD

为了满足对高能中子辐射场测量仪器进行校准的需要,必需建立20MeV以上的准单能中子参考辐射场.对国际上（20～400） MeV准单能中子参考辐射场的建立情况及建立方法进行了调研,可通过7Li（p,n）7Be反应获得该能区准单能中子场,中子束流轮廓可通过转换体和影像板进行测量,辐射场中子能谱可利用液体闪烁探测器或者238U裂变电离室通过飞行时间法进行测量,可建立高效率的反冲质子望远镜作为该能区的中子注量测量初级标准.     

FUZZY IDENTIFICATION METHOD BASED ON A NEW OBJECTIVE FUNCTION

Many fuzzy models on modeling and controlmethods have been developed since Takagi-Sugeno model was proposed[1] .The main prob-lems of the fuzzy identifying method based on T-S model appear in the following two aspects:　　 1 It is important what heuristic knowledgeis chosen to acquire the premise structure of theT- S model.This problem is related to the opti-mal partition of input space of premise part andmodeling accuracy.　　 2 Itis crucial whatidentifying method is u-tilized to estimate …     

Analysis of the DORIS contributions to ITRF2008

In its function as an ITRS Combination Centre, DGFI is in charge with the computation of an ITRF2008 solution. The computation methodology of DGFI is based on the combination of datum-free normal equations (weekly or session data sets, respectively) of station positions and Earth orientation parameters (EOP) from the geodetic space techniques DORIS, GPS, SLR and VLBI. In this paper we focus on the DORIS part within the ITRF2008 computations. We present results obtained from the analysis of the DORIS time series for station positions, network translation and scale parameters, as well as for the terrestrial pole coordinates. The submissions to ITRF2008 benefit from improved analysis strategies of the seven contributing IDS analysis centres and from a combination of the weekly solutions of station positions and polar motion. The results show an improvement by a factor of two compared to past DORIS data submitted to ITRF2005, which has been evaluated by investigating the repeatabilities of position time series. The DORIS position time series were analysed w.r.t. discontinuities and other non-linear effects such as seasonal variations. About 40 discontinuities have been identified which have been compared with the results of an earlier study. Within the inter-technique combination we focus on the DORIS contribution to the integration of the different space geodetic observations and on a comparison of the geodetic local ties with the space geodetic solutions. Results are given for the 41 co-location sites between DORIS and GPS.     

基于FDG和GA的故障诊断技术在电子对抗装备中的应用

探讨了模糊有向图（Fuzzy Directed Graph,FDG）和遗传算法（Genetic Algorithm,GA）相结合的故障诊断技术及其在电子对抗装备故障诊断中的具体应用。根据电子对抗装备组件的实际状态,应用模糊理论得出各组件发生故障的可能性,建立电子对抗装备的模糊有向图,利用遗传算法搜索出模糊有向图中可能的故障传播路径。实践表明,该技术应用在电子对抗装备的故障诊断中是行之有效的,取得了较好的诊断结果。     

试用暗物质理论解释惯性和惯性力的物理机制(上)

基于对暗物质的多年探讨,我们认为宇宙空间是具有质量、相对均匀、连续稳定和有相当弹性暗物质群体(DMG)的空间.自然、宇宙万物终生处于群体引力制约之中,它们因此也获得了相应的惯性.本文立足于上述的宇宙空间,借助宇宙学原理、马赫原理和爱因斯坦等效原理,提出了物质客体的惯性机制和被称为虚力的惯性力机制 同时本文也解读所有惯...     

A few metrological aspects of the Gaia mission

The ESA space astrometry mission Gaia is designed to measure the positions, parallaxes and proper motions of more than one billion stars of our Galaxy brighter than 20 magnitude. The expected astrometric accuracies are in the range 7–25 μas for the point-like sources down to 15 mag. To achieve this staggering performance, several issues of highly accurate metrology must be solved and implemented on the spacecraft. In this paper, I discuss first some constraining principles to perform global astrometry in space, and then a couple of examples of the metrological issues currently faced by the design or to be encountered during the operations. One concerns the optimisation of the sky coverage with a scanning instrument like Gaia, and the other deals with the instrument stability and how the stringent requirements are met in practice.