Instability of the present LEO satellite populations

Several studies conducted during 1991–2001 demonstrated, with some assumed launch rates, the future unintended growth potential of the Earth satellite population, resulting from random, accidental collisions among resident space objects. In some low Earth orbit (LEO) altitude regimes where the number density of satellites is above a critical spatial density, the production rate of new breakup debris due to collisions would exceed the loss of objects due to orbital decay.     

改进的完备模态型减缩法

一种经过改进的完备模态型减缩法成功地本文提出来了。它有效地克服了原完备模态型减缩法不能保持自由结构之刚体特性的缺点，可是由ＩＣＭＲ法产生的减缩模型的弹性模态精度却不及ＣＭＲ法。     

测量中单输入单输出线性系统动态数学模型定阶方法的仿真研究

针对测量中单输入单输出线性系统的动态建模问题,通过计算机数字仿真,对现有的几种定阶方法进行了研究、分析,比较了它们在不同信噪比、不同数据长度、不同模型情况下模型定阶的可靠性、等价性和选择原则,并得到了一些重要的结论。     

Parametric study of turbine NGV blade lean and vortex design

The effects of blade lean and vortex design on the aerodynamics of a turbine entry nozzle guide vane (NGV) are considered using computational fluid dynamics. The aim of the work is to address some of the uncertainties which have arisen from previous studies where conflicting results have been reported for the effect on the NGV. The configuration was initially based on the energy efficient engine turbine which also served as the validation case for the computational method. A total of 17 NGV configurations were evaluated to study the effects of lean and vortex design on row efficiency and secondary kinetic energy. The distribution of mass flow ratio is introduced as an additional factor in the assessment of blade lean effects. The results show that in the turbine entry NGV, the secondary flow strength is not a dominant factor that determines NGV losses and therefore the changes of loading distribution due to blade lean and the associated loss mecha-nisms should be regarded as a key factor. Radial mass flow redistribution under different NGV lean and twist is demonstrated as an addition key factor influencing row efficiency.     

Modeling and simulation of bow wave effect in probe and drogue aerial refueling

In a probe and drogue aerial refueling system, the bow wave of the receiver aircraft will produce a strong aerodynamic effect on the drogue once the receiver follows the drogue at a close distance. It is a major difficulty of docking control in the probe and drogue refueling. This paper analyses the bow wave effect and presents a simple method to model it. Firstly, the inviscid flow around the receiver is modeled based on the stream function defined by basic stream singularities.Secondly, a correction function is developed to eliminate the error caused by the absence of air viscosity. Then, the aerodynamic coefficients are used to calculate the induced aerodynamic force on the drogue. The obtained model is in an analytical form that can be easily applied to the controller design and the real-time simulations. In the verification part, computational fluid dynamics(CFD)simulation tests are conducted to validate the obtained flow fields and aerodynamic forces. Finally,the modeling method is applied to an F-16 receiver aircraft in a previously developed autonomous aerial refueling simulation system. The simulations results are analyzed and compared with the NASA flight-test data, which demonstrates the effectiveness of the proposed method.     

基于UML的自动测试系统建模方法研究

为提供自动测试系统的领域知识，在对自动测试系统的特性进行研究的基础上，将UML引入自动测试系统的建模过程中，利用UML的扩展机制为自动测试系统的框架开发提供该领域的知识。通过为一个自动测试系统开发平台不同于常规软件产品部分的建模实例，给出了自动测试系统的特定领域知识的表达方式。     

基于Pro/E的双轴定位机构虚拟样机的建模与校核

介绍了在Pro/E设计平台上完成某卫星天线双轴定位机构虚拟样机模型的建模、仿真与校核。根据该定位机构的特点,建立了虚拟样机模型并完成静态校核。通过设定必要的参数值,对虚拟样机作包括运动学和动力学仿真的动态校核。由仿真结果与规定设计指标的比较可知,该虚拟样机符合设计要求。     

飞行器合理传递参数的解法

本文基于矢量矩阵分析法,建立了含气动、结构和飞行参数及其偏量的数学模型,它可用来分析飞行器的合理传递参数。按此方法不仅可以同时调整若干设计参数,而且还可简化计算机辅助设计的程序。为选择合理传递参数,列出了设计参数的调整准则。 取用动态因子和转换因子,使所得方法对于正常式、鸭式、旋转弹翼式和弹道式导弹都是适用的。     

一种新的硬/软件系统可靠性分析方法

在一种新的软件可靠性分析方法基础上，参考硬件系统的阶段性任务可靠性的建方法，为在对于不可修的计算机系统进行可靠性分析时考虑硬、软件之间复杂的相关作用提出了一套比较全面的解决办法。从而为更准确地评估计算机系统可靠性提供了可能。文中分析了一个飞行控制系统实例。     

Longitudinal behaviors of the IRI-B parameters of the equatorial electron density profiles retrieved from FORMOSAT-3/COSMIC radio occultation measurements

The electron density profiles in the bottomside F₂-layer ionosphere are described by the thickness parameter B0 and the shape parameter B1 in the International Reference Ionosphere (IRI) model. We collected the ionospheric electron density (N_e) profiles from the FORMOSAT-3/COSMIC (F3/C) radio occultation measurements from DoY (day number of year) 194, 2006 to DoY 293, 2008 to investigate the daytime behaviors of IRI-B parameters (B0 and B1) in the equatorial regions. Our fittings confirm that the IRI bottomside profile function can well describe the averaged profiles in the bottomside ionosphere. Analysis of the equatorial electron density profile datasets provides unprecedented detail of the behaviors of B0 and B1 parameters in equatorial regions at low solar activity. The longitudinal averaged B1 has values comparable with IRI-2007 while it shows little seasonal variation. In contrast, the observed B0 presents semiannual variation with maxima in solstice months and minima in equinox months, which is not reproduced by IRI-2007. Moreover, there are complicated longitudinal variations of B0 with patterns varying with seasons. Peaks are distinct in the wave-like longitudinal structure of B0 in equinox months. An outstanding feature is that a stable peak appears around 100°E in four seasons. The significant longitudinal variation of B0 provides challenges for further improving the presentations of the bottomside ionosphere in IRI.