从具有非线性特征的衰减“拍”波形确定阻尼率的方法

本文提出一个从具有非线性特征的衰减“拍”波形确定阻尼率的方法——二次包络法。第一次包络是对衰减“拍”波形实施希尔伯特(Hilbert)变换得到的,第二次包络是以第一次包络曲线的峰谷值为基准,分段用线性插值形成的变系数指数曲线。根据第二次包络的两条曲线,用对数减量确定随响应振幅而变的阻尼率。本文以分离贮箱中液体晃动阻尼的确定为例验证了方法,结果表明精度达到了工程应用的程度。除对液体晃动的阻尼测定之外,本方法还适用于密模态高粘弹性结构的模态阻尼测定。     

航空电子设备安装支架的刚度与频率优化设计

航空电子设备用于飞行中的数据采集,通常使用安装支架固定于机头雷达罩,研究安装支架的刚度和一阶频率性能,避免设备支架在飞行过程中出现塑性变形和共振现象,对提高飞行稳定性具有重要的工程意义。在惯性载荷下对安装支架进行静强度和模态分析,采用一种灵敏度分析方法确定安装支架的设计变量,以结构总质量最小为优化目标,在保证安装支架的刚度和一阶模态性能的前提下对支架各个构件的厚度进行优化设计,并对优化后的安装支架结构进行振动试验。结果表明：优化后的安装支架结构刚度基本保持不变,一阶频率提高了18.09%,质量减少了19.33%,改进设计满足设备安装要求。     

航天器多普勒测速平均误差的分析与修正

对航天器多普勒测速平均误差进行了分析,详细推导了圆轨道和椭圆轨道时该误差的计算公式,计算了不同采样周期和轨道高度时的误差大小。经过分析指出,该项误差对于高轨航天器影响较小,对于低轨航天器可以通过缩短采样周期或利用3个点或多个点的连续测量数据进行修正。     

基于视图的试验通信需求分析方法研究

针对试验通信系统规划中的需求分析工程化问题,按照体系结构方法的要求,提出了一种基于视图的信息需求获取及分析处理方法;该方法能够在一定程度上简化和规范化需求获取,并通过一系列分析步骤实现从试验要素和任务向试验信息流的转化。     

Proposal of new models of the bottom-side B0 and B1 parameters for IRI

The time series of hourly electron density profiles N(h) obtained from 27 ionosonde stations distributed world-wide have been used to obtain N(h) average profiles on a monthly basis and to extract the expected bottom-side parameters that define the IRI profile under quiet conditions. The time series embrace the time interval from 1998 to 2006, which practically contains the entire solar cycle 23. The Spherical Harmonic Analysis (SHA) has been used as an analytical technique for modeling globally the B0 and B1 parameters as general functions on a spherical surface. Due to the irregular longitudinal distribution of the stations over the globe, it has been assumed that the ionosphere remains approximately constant in form for a given day under quiet conditions for a particular coordinate system. Since the Earth rotates under a Sun-fixed system, the time differences have been considered to be equivalent to longitude differences. The time dependence has been represented by a two-degree Fourier expansion to model the annual and semiannual variations and the year-by-year analyses of the B0 and B1 have furnished nine sets of spherical harmonic coefficients for each parameter. The spatial–temporal yearly coefficients have been further expressed as linear functions of Rz12 to model the solar cycle dependence. The resultant analytical model provides a tool to predict B0 and B1 at any location distributed among the used range of latitudes (70°N–50°S) and at any time that improves the fit to the observed data with respect to IRI prediction.     

Contributions of the French Institut Géographique National (IGN) to the International DORIS Service

DORIS is one of the four geodetic space techniques participating to the Global Geodetic Observing System (GGOS). Since the early development of this system, the Institut Géographique National played a specific and active role. Within, the International DORIS Service (IDS), IGN is in a particular position. While it is responsible for the installation and the maintenance of the DORIS ground tracking stations, it also handles one of the two IDS data center delivering DORIS data and products and has been an IDS Analysis Center for years, providing all possible IDS products, in particular the latest ignwd08 time series in preparation of ITRF2008. This paper explains the different aspects of the IGN contribution to IDS from an historical point of view, presents current activities and scientific results and provides a perspective for future activities. Recent DORIS results show a 10 mm precision or better when more than four DORIS satellites are available. Comparisons between recent DORIS solutions (ign07d02 and ign09d02) and past ITRF realizations show that errors are shared between the DORIS and the ITRF realizations. Some problems related to DORIS data processing are also discussed and possible ways to solve them in the future are discussed. In particular, we can now reject the tropospheric origin of the problem detected in the Envisat data after the software upload of October 12, 2004. A few applications in geodesy (terrestrial reference frame, Earth’s polar motion) and geophysics are also discussed as a natural extension of these service-type activities.     

重排算法在多目标雷达信号分辨中的应用

本文使用１５年前由柯德锐等人首次在谱图中使用,并经弗朗克斯等人改进并推广的重排算法,对多目标雷达信号进行架次识别,此重排算法简单且极易实施,在重排后失支双线性时,却保持了其他许多可取特性,并换回了Ｃｈｉｒｐ信号和冲击信号的准确定位,针对编队多目标雷达信号的线性调频特点,利用此重排算法在权衡能量聚集性和消重排振荡的同时,实现了对编队多目标雷达信号的分辨。     

船只目标三维转动对SAR成像影响的定量分析

在分析船只三维转动（横滚、俯仰、偏航）对合成孔径雷达（Synthetic Aperture Radar,SAR）成像质量的影响方面,现有文献只考虑了仅存在一维转动时的影响,未考虑三维转动同时存在时对SAR成像质量的影响。另外,现有文献主要基于船只转动对船只散射点瞬时多普勒频率的影响进行分析,并未真正与对SAR图像质量的影响关联起来。本文推导了适用于船只存在三种一维转动、同时存在三维转动时的SAR图像二维时域表达式,以及散射点方位向坐标的表达式。在上述表达式的基础上,通过分析船只上的散射点在SAR图像中的偏移情况,扩展到分析船只整体在SAR图像中的形变情况;通过分析一维转动对SAR成像的影响,扩展到分析三维转动同时存在时对SAR成像的影响。研究表明：船只三维转动引入了包络误差和相位误差,导致SAR图像中散射点模糊并在方位向偏移,且不同散射点的偏移量不同,从而使船只形状发生畸变。仿真结果验证了所推导表达式的准确性及理论分析的正确性。     

高推重比航空发动机调节规律分析

针对先进高推重比涡扇发动机采用的调节规律进行了研究。通过对采用不同调节规律下的混合加力涡扇发动机非安装性能进行对比,分析了高推重比发动机采用的调节规律的优越性。     

空间光学遥感器扫描运动部件运动学与动力学分析方法研究

利用CAE的建模及仿真技术并应用运动学和多体动力学分析软件 (RecurDyn)与结构力学分析软件 (Nastran)相结合的分析研究方法为解决某类带扫描运动部件的空间光学遥感器的运动特性分析及设计提供了参考 ,对该运动机构设计的合理性进行了初步分析评估