大型可展开天线太空结构频率预测

由于空间大型可展开天线口径较大,在地面模拟太空环境难度高,使得直接在天线原型上进行性能测试非常困难或不可能。为了解决该问题,提出了一种“两步法”,利用空间大型可展开天线的缩比模型进行地面性能测试,以预测天线原型在太空中的工作性能。据此对周边桁架可展开天线太空工作的结构固有频率进行性能预测研究,首先推导了结构固有频率的相似准则,然后考虑结构参数畸变的影响,得出其相似性经验公式,最后研究了温度变化对结构频率的影响,得出了预测大型天线太空工作性能的经验公式。仿真结果验证了该方法的有效性,该方法可应用于其他空间结构的设计和性能预测。     

双峰应力谱密度雨流幅值分布

为了在频域内解决双峰应力谱密度下的结构疲劳寿命估算问题,提出了双峰应力谱的雨流幅值分布模型,并给出了参数估算方法。假设雨流幅值分布为两个双参数Weibull分布的组合,权重系数反映了两个谱密度峰值对雨流幅值分布的贡献;雨流幅值分布模型中的参数均是随机过程谱参数的函数。数值模拟结果表明：两个Weibull分布的组合能够很好地描述双峰应力谱的雨流幅值分布,模型中的参数能够根据双峰应力谱密度的谱参数计算得出。     

基于模糊逻辑系统的转子振动控制方法研究

电流变液作为一种智能材料在振动控制工程领域有着广泛的应用。由于电流变效应具有非线性特性,使得难以设计基于常规控制理论的控制律。本文利用模糊逻辑系统能够逼近非线性函数的特性,设计了电流变阻尼器-转子振动系统自适应模糊控制方案。针对该转子系统的仿真计算表明,转子系统的振幅能够得到有效的抑制,自适应模糊控制器性能良好。      

一种基于小波零树的彩色图像编码算法

为提高基于分层树的集合分割算法(SPIHT)的编解码速度,对算法结构重新设计,提出了一种简单的无链表小波零树编码算法.通过预处理和主处理过程实现了流水线编码结构,减少了存储器的访问频率.预处理完成对所有节点显著性的标注,主处理完成无链表的零树编码.对彩色图像编码时首先进行RGB空间到YUV空间的变换,然后在比特平面扫描过程中,依次对YUV三个平面进行编码,这样输出的码流是完全嵌入式的.一般情况下,亮度分量的最高显著平面都高于色度分量.因此通过色度分量输出控制策略,可以进一步提高算法对彩色图像的编码性能.硬件实现结果表明,改进后算法的编解码速度明显提高,而率失真性能并没有下降,所以新算法特别适合高分辨率或不规则图像的编解码芯片设计.     

半球型介质加载的单极子天线的全波分析

对轴对称柱坐标的时域有限差分方法进行了详细的讨论 ,并将完全匹配层吸收边界条件推广到圆柱坐标系。使用时域有限差分方法对半球型介质加载的单极子天线进行了全波分析 ,给出了其S参数曲线和输入阻抗的数值计算结果 ,并与文献结果进行了比较 ,吻合较好。     

环绕智能系统架构设计及身份感知Agent实现

介绍了环绕智能(AmI, Ambient Intelligence)的概念,分析了AmI系统中上下文感知数据流,提出了基于多Agent系统(MAS, Multi-Agent System)的AmI系统架构.详细介绍了在此架构基础上设计实现的具有上下文感知的AmI实验系统-AmI-Space,并对其中的用户感知Agent进行了描述.实验证明,基于MAS的AmI系统架构满足了AmI系统中计算单元的模块化、分散化、可变性和复杂性要求;同时AmI-Space中的用户感知Agent结合了蓝牙Ad hoc网和以太网的优点,实现了一种无需用户配合的身份感知机制,是一种自然的、主动的交互方式.      

喷雾冷却系统稳态特性的实验研究

设计了一套可观察喷雾过程中的喷雾锥角、雾化效果、发热面上液膜及腔内气液分布状态的实验系统。验证了喷雾冷却技术解决极高热流密度散热问题的能力。通过实验研究了该系统的传热性能与稳态运行特性,分析了流量、喷嘴压降、喷雾高度、热流密度、热沉温度及回流液体过冷度等因素对系统传热性能和特性的影响。     

The solar cycle variation of plasma parameters in equatorial and mid latitudinal areas during 2005–2010

Based on the ISL data detected by DEMETER satellite, the solar cycle variation in electron density (Ne) and electron temperature (Te) were studied separately in local daytime 10:30 and nighttime 22:30 during 2005–2010 in the 23rd/24th solar cycles. The semi-annual, annual periods and decreasing trend with the descending solar activity were clearly revealed in Ne. At middle and high latitudes, there exhibited phase shift and even reversed annual variation over Southern and Northern hemisphere, and the annual variation amplitudes were asymmetrical at both hemispheres in local daytime. In local nighttime, the annual variations of Ne at south and north hemispheres were symmetrical at same latitudes, but the annual variation amplitudes at different latitudes differed largely, showing obviously zonal features. As for Te, the phase shift in annual variations was not as apparent as Ne with the increase of latitudes at Southern and Northern hemisphere in local daytime. While in local nighttime the reversed annual variations of Te were shown at low latitudinal areas, not at high latitudes as those in Ne. The correlation study on Ne and Te illustrated that, in local daytime, Ne and Te showed strong negative correlation at equator and low latitudes, but during the solar minimum years the correlation between Ne and Te changed to be positive at 25–30° latitudes in March 2009. The correlation coefficient R between Ne and Te also showed semi-annual periodical variations during 2005–2010. While in local nighttime, Ne and Te exhibited relatively weak positive correlation with R being about 0.6 at low latitudes, however no correlation beyond latitudes of 25° was obtained.     

Sliding mode tracking control for miniature unmanned helicopters

A sliding mode control design for a miniature unmanned helicopter is presented. The control objective is to let the helicopter track some predefined velocity and yaw trajectories. A new sliding mode control design method is developed based on a linearized dynamic model. In order to facilitate the control design, the helicopter’s dynamic model is divided into two subsystems,such as the longitudinal-lateral and the heading-heave subsystem. The proposed controller employs sliding mode control technique to compensate for the immeasurable flapping angles’ dynamic effects and external disturbances. The global asymptotic stability(GAS) of the closed-loop system is proved by the Lyapunov based stability analysis. Numerical simulations demonstrate that the proposed controller can achieve superior tracking performance compared with the proportionalintegral-derivative(PID) and linear-quadratic regulator(LQR) cascaded controller in the presence of wind gust disturbances.     

基于励磁电流前馈调节的航空直流发电系统建模分析

 高压直流(HVDC)发电系统因为其效率高、质量轻以及可靠性高等诸多优点成为航空供电系统的首选,其系统输出端存在着用于滤波的大电容,这使得采用传统PI调节方案的调压器不能满足系统的动态性能要求。因此,提出了采用励磁电流前馈(ECF)的调压器技术。对该技术进行了详细的理论分析,分别建立了有励磁电流前馈环和无励磁电流前馈环的发电系统的数学模型。比较2个系统的性能,发现有励磁电流前馈环的发电系统截止频率得到了较大的提高。实验表明,在突加负载和突卸负载2种情况下,加入励磁电流前馈环控制,系统能够迅速响应,保持稳定并且超调量小,动态性能得到了明显提高。该方法可推广到不同类型的航空发电系统的调压控制中。