基于蚁群算法的多任务导航星座载荷配置

给出了多任务导航星座载荷配置的一套新算法.首先建立了多任务导航星座载荷配置的优化模型;基于任务要求定义并提出了n＋1重覆盖率来评价星座对地面的覆盖性能;蚁群算法(ACA)是一种新型的模拟蚂蚁觅食行为的仿生启发式算法,将蚁群算法运用到载荷配置的优化当中,修正了启发函数及Ant-Cycle模型使它们能够与星座载荷配置的优化相结合;给出了基于该算法的多任务载荷配置优化框图.仿真结果表明蚁群算法快速有效,优化结果满足任务要求.      

基于Weibull分布的疲劳加速腐蚀因子分析

考虑预腐蚀对飞机结构疲劳寿命的影响,建立了疲劳寿命服从Weibull分布的 加速腐蚀因子确定方法.假设预腐蚀疲劳寿命服从Weibull分布,特征寿命随时间呈指数规 律变化,推导得到了以疲劳寿命为腐蚀量的加速腐蚀因子表达式,以及在工程常用的时间范 围内加速腐蚀因子与腐蚀时间无关的结论;进行了相关参数估计,建立了加速腐蚀 因子的估计方法,得到了加速腐蚀因子估计量的近似分布,对其进行了统计分析.      

一次砝码国际比对

介绍了中国航空长城计量测试研究所质量校准实验室参加亚太地区国际实验室之间砝码比对的情况,给出了测量结果的不确定度分析。     

星载合成孔径雷达的一种新波形及其处理技术

分析研究了步进频率脉冲串信号在星载合成孔径雷达 (SAR)中应用时的多普勒效应 ,并提出了一种纵向距离合成高分辨成像时多普勒二次相位的补偿方法 ,从而消除了纵向距离分辨率的恶化和信噪比损失 ,同时还可以消除纵向距离向与方位向之间的多普勒耦合     

一种无人机通用综合检测系统

为了增强无人机系统检测控制设备的通用性,提高检测精度,设计了一种基于面向仪器系统的PCI扩展(PXI)总线及虚拟仪器(VI)的无人机通用综合检测系统.针对无人机系统工作的特点,从功能设计、体系结构、软硬件设计等方面对该系统的通用性进行了探讨.该系统采用了虚拟仪器技术,硬件设计采用PXI体系结构,软件以LabWindows/CVI作为开发平台.通过配备不同的接口适配器和对软件参数设置进行相应更改,可适用于不同型号的无人机电气、舵机、发动机、起飞和回收等系统检测.同时提供矩阵输出,利用系统资源满足无人机各种信号测试/激励的需求.该系统已成功应用于某复杂型号无人机的地面综合检测.      

微系统Interposer测试技术与发展趋势

随着微系统技术向三维立体集成不断发展,Interposer技术逐渐成为关注的焦点,是未来电子系统小型化和多功能化的重要技术途径,具有广阔的应用市场和发展前景。关于Interposer的测试技术研究也提上发展日程。对目前Interposer测试技术的研究现状和发展趋势进行了综述,重点总结了研究机构在Interposer测试技术领域的研究现状,并对技术发展趋势做了简单展望。     

Parallel algorithm and its convergence of spatial domain decomposition of discrete ordinates method for solving radiation heat transfer problem

To improve the computational efficiency and hold calculation accuracy at the same time,we study the parallel computation for radiation heat transfer. In this paper, the discrete ordinates method(DOM) and the spatial domain decomposition parallelization(DDP) are combined by message passing interface(MPI) language. The DDP–DOM computation of the radiation heat transfer within the rectangular furnace is described. When the result of DDP–DOM along one-dimensional direction is compared with that along multi-dimensional directions, it is found that the result of the latter one has higher precision without considering the medium scattering. Meanwhile, an in-depth study of the convergence of DDP–DOM for radiation heat transfer is made. Analyzing the cause of the weak convergence, we relate the total number of iteration steps when the convergence is obtained to the number of sub-domains. When we decompose the spatial domain along one-,two- and three-dimensional directions, different linear relationships between the number of total iteration steps and the number of sub-domains will be possessed separately, then several equations are developed to show the relationships. Using the equations, some phenomena in DDP–DOM can be made clear easily. At the same time, the correctness of the equations is verified.     

Theoretical study of flow ripple for an aviation axial-piston pump with damping holes in the valve plate

Based on the structure of a certain type of aviation axial-piston pump＇s valve plate which adopts a pre-pressurization fluid path （consisting a damping hole, a buffer chamber, and an orifice） to reduce flow ripple, a single-piston model of the aviation axial-piston pump is presented. This sin- gle-piston model comprehensively considers fluid compressibility, orifice restriction effect, fluid resistance in the capillary tube, and the leakage flow. Besides, the instantaneous discharge areas used in the single-piston model have been calculated in detail. Based on the single-piston model, a multi-piston pump model has been established according to the simple hydraulic circuit. The sin- gle- and multi-piston pump models have been realized by the S-function in Matlab/Simulink. The developed multi-piston pump model has been validated by being compared with the numerical result by computational fluid dynamic （CFD）. The effects of the pre-pressurization fluid path on the flow ripple and the instantaneous pressure in the piston chamber have been studied and opti- mized design recommendations for the aviation axial-piston pump have been given out.     

一种载人小行星探测目标星初选方法

针对载人小行星探测任务目标选取问题,通过对目标星选取影响因素的定量分析,提出了目标星初选方案。首先根据火箭的运载能力提出目标星轨道参数的筛选条件,然后根据地面观测和尺寸约束提出目标星绝对星等的要求,再根据结构的稳定性和温控要求提出目标星自旋周期的范围,最后按照科学价值并综合考虑其他因素建立目标星选取优化模型,得出目标星优选序列。根据提出的目标星初选方案和具体的任务需求进行载人小行星探测目标星选取,得出了目标星优选序列,证明了该方案合理、有效,为载人小行星探测提供一定的技术参考。     

大气对遥感卫星图像品质的影响分析

影响遥感卫星图像品质的因素很多,其中包括成像条件中的大气辐射.文章根据遥感成像理论分析了大气辐射对遥感卫星图像品质的影响,计算了大气背景及大气对图像层次和图像对比度的影响.最后,结合遥感相机的特点,给出了减少大气影响、提高图像品质的建议.