滤波器的相频特性对像质影响的仿真

利用计算机仿真的方法,研究了椭圆低通滤波器和Butterworth滤波器的相频特性对像质的影响。这种影响主要有边缘退化、分辨率损失、产生新的干扰条纹和几何畸变以及多波段图像配准精度降低等。     

卫星摄影系统象移补偿速高比计算

本文研究了卫星摄影系统象移补偿速高比计算。从飞机上拍摄地面景物时,象移补偿速高此中的速度为地面相对飞机的速度,通常称为地速。但是,从卫星上拍摄地面照片时,如果把速高比中的速度取为地面相对于卫星的速度,则会导出谬误。为此,作者对速高比的定义进行了推广,对于这种拓广的速高比定义,也能适用于从飞机上拍摄地面景物的速高比计算。本文在推导公式过程中,把地球视为旋转椭球体,卫星轨道为椭圆轨道,导出了计算星下点速度和速高比的公式。最后与把地球视为正球体,忽略轨道偏心率的计算结果相比较,速高比的相对误差不超过0.5%。     

涡轮盘双工位精密侧拉床研制

本文概述了WK-PCL2025型微机控制双工位精密侧拉床的设计特点及技术性能,着重介绍了拉床所采用的新结构导轨系统。试验证明,该拉床液压系统低速性能较好,试拉的涡轮盘榫齿满足设计要求。     

On compositional variations of heavy ions during solar particle events

Intensity-time profiles of protons, alpha particles, and heavy ions (C, O, Fe) in the MeV/nucleon energy range have been analyzed for one solar particle event following the solar flare on September 23, 1978. The data have been obtained with the wide angle double dE/dx-E sensor of the Max-Planck-Institut/University of Maryland experiment onboard ISEE-3. We found time variations in the iron to helium ratio of up to 2 orders of magnitude and a significant variation of the O/He ratio during this event, whereas the C/O-ratio at the same energy/nucleon appears to be time independent. We investigated the influence of a rigidity dependent mean free path in interplanetary space and of rigidity dependent coronal propagation on heavy ion ratios during solar particle events. We found that both the magnitude and time scale of the ratio changes during the September 23 event cannot be explained by rigidity dependent interplanetary or coronal propagation alone. These ratio changes are probably caused by multiple injection at the sun.     

在专业人才培养上的一个新尝试

本文就改革原教学模式,走继续工程教育和企校挂钩联合办学的道路,突出教学为生产服务的原则,尝试了一种新的办学方式,即:继续工程教育“4 1”和联合办学的“3 1”模式,进行了简明扼要的论述。     

非均匀流场中燃油浓度测量的试验技术

本文设计了在非均匀流场中,能同时测量其速度分布、浓度分布和温度分布的取样感头,建立了相应的测试系统,分析讨论了该系统的测量精度及其影响因素。在常温和高温气流作用下,测量了非均匀流场中燃油浓度分布、速度分布及温度分布。燃油浓度在常温时误差在±10％以内,高温时误差在±6％以内。     

基于STK的星敏感器在轨视场仿真分析

针对星敏感器在轨可能会受到太阳光、地气光等杂光干扰而影响其测量精度及姿态有效率等问题,对星敏感器的在轨视场进行了分析研究。给出了太阳光、地气光进入星敏感器视场的条件;基于卫星工具包(STK)软件,提出了一种星敏感器视场分析的仿真方法;结合卫星轨道参数和星敏感器安装方位,在卫星零姿态、正负向侧摆下对杂光进入星敏感器视场情况进行了仿真。结果表明,卫星在轨至少有2个星敏感器在同一时刻满足杂光抑制角要求。文章提出的仿真方法,适用于对任何轨道类型卫星星敏感器在轨视场的杂光分析,仿真结果对星敏感器在卫星上的优化安装具有工程应用价值。     

Bifurcation analysis of polynomial models for longitudinal motion at high angle of attack

To investigate the longitudinal motion stability of aircraft maneuvers conveniently, a new stability analysis approach is presented in this paper. Based on describing longitudinal aerodynamics at high angle-of-attack (a < 50 ) motion by polynomials, a union structure of two-order differential equation is suggested. By means of nonlinear theory and method, analytical and global bifurcation analyses of the polynomial differential systems are provided for the study of the nonlinear phenomena of high angle-of-attack flight. Applying the theories of bifurcations, many kinds of bifurcations, such as equilibrium, Hopf, homoclinic (heteroclinic) orbit and double limit cycle bifurcations are discussed and the existence conditions for these bifurcations as well as formulas for calculating bifurcation curves are derived. The bifurcation curves divide the parameter plane into several regions; moreover, the complete bifurcation diagrams and phase portraits in different regions are obtained. Finally, our conclusions are applied to analyzing the stability and bifurcations of a practical example of a high angle-of-attack flight as well as the effects of elevator deflection on the asymptotic stability regions of equilibrium. The model and analytical methods presented in this paper can be used to study the nonlinear flight dynamic of longitudinal stall at high angle of attack.     

基于旋转阀的脉冲爆震火箭发动机实验

针对现有条件下电磁阀高频与大流量不可兼得的矛盾,设计了一种凸轮式旋转阀,以此来控制脉冲爆震火箭发动机氧化剂、燃料和隔离气体的间歇式供给.基于该旋转阀,以汽油和富氧空气为推进剂,进行了不同频率下的实验.实验结果表明,推进剂和隔离气供给压力与点火相位直接影响到能否稳定起爆.随着频率的增加,在1～ 10 Hz范围内,降低隔离氮气压力、调整点火相位可实现发动机的稳定工作;10Hz以上时,仅需要提高油气的供给压力.基于该旋转阀控制技术,脉冲爆震火箭发动机实现了工作频率30 Hz的稳定工作.     

SiO2 气凝胶热参数测试及评价

利用非稳态阶跃平面热源法对SiO2气凝胶的热参数进行了高温实验研究,获得了不同温度和压力条件下SiO2气凝胶的热导率、热扩散率以及比热容等.结果表明,SiO2气凝胶800℃的热导率比室温增大约62％.在相同气压且低于600℃时,其热导率受比热容影响,而在高于600℃时,则受热扩散率影响;在相同温度且高于10 kPa时,热导率亦受热扩散率影响.