基于1773光纤数据总线的光传飞控系统

为完成直升机显模型跟踪光传飞控系统局域网的设计,对基于 MIL-STD-1533B多路传输数据总线协议的 MIL-STD-1773光总线协议进行了研究;提出了基于1773光总线的光传系统的开发思想和途径,并对光总线的硬件结构配置及软件实现进行了设计;构建了直升机显模型跟踪光传操纵系统的地面物理仿真验证平台,由给出的光传与电传对比仿真,表明所设计系统是正确并可行的,对开发光传操纵技术具有工程意义。     

CFM56-5B发动机推力管理及一起故障分析

系统地阐述了CFM56-5B发动机推力管理和慢车转速控制的工作原理,并以此为基础,针对该型发动机一起常见推力控制故障的现象、原因及其排故方法进行了分析。通过此分析,进一步说明了CFM56-5B发动机慢车转速控制的基本控制逻辑,可为航空公司正确处理此类故障提供参考。     

基于1553B总线的惯导系统终端设计

为了适应惯导系统数据传输的实时性和可靠性的需求,本文提出了基于1553B总线的惯导系统数据采集和传输方案.文章描述了1553B总线终端接口芯片BU-61580的内部寄存器和RAM资源,提出了BU-61580与TMS320F206 DSP芯片的硬件接口设计和软件接口设计方案.实现了1553B终端RT与总线控制器BC之间的...     

Spatial asymmetry in topside ion density and vertical E × B plasma drift velocity within 75°E–95°E

The ion density measured by the Ionospheric Plasma and Electrodynamics Instrument (IPEI) on board the ROCSAT -1 over the 75°E and 95°E meridian at 600km altitude has been utilized to examine the latitudinal and longitudinal distribution within the Indian sector, in particular, the north-south and east-west asymmetries of the equatorial ionization anomaly (EIA). A longitudinal gradient in ion density at 600?km higher towards 95°E develops during the noontime and afternoon hours when the EIA is at its peak. The density gradient persists till evening hours when pre-reversal enhancements occur. The vertical E?×?B plasma drift velocity measured simultaneously by ROCSAT -1 for the same space-time configuration has also been studied. In addition to diurnal, seasonal and solar activity variations in E?×?B drift velocity, the longitudinal gradient is also observed. The EIA at the altitude of 600?km peaks at different latitudes and are mostly asymmetric about the magnetic equator. From midnight till 0800 LT, the ion density across the equator is nearly uniform in the equinoxes. But in the solstices, the density exhibits a north-south gradient. In the June solstice, density is higher in the northern hemisphere and decreases gradually towards south. The gradient in density reverses in December solstice. Normally, the EIA peaks within 1200 LT and 1600 LT while around 2000 LT, pre-reversal enhancement of ionization occurs affecting the EIA evening structure. The strength of the EIA also exhibits seasonal, year-to-year and hemispheric variations. The longitudinal asymmetry of drift velocity along 75°E and 95°E longitude sectors is the contributing factor behind the observed longitudinal asymmetry in ion density. Significant positive correlation between the strength of the EIA and E?×?B drift is observed in both longitudes.     

集装箱甩挂运输模型与应用

描述了集装箱甩挂运输的作业流程.从车辆等待时间的角度及集装箱甩挂运输的特点,分析了集装箱甩挂运输在不同情况的适用性问题.使用0-1决策变量来描述集装箱甩挂运输的各个操作流程,建立了以提箱次数、放箱次数、行驶次数、等待时间及各项操作流程的发生顺序为约束条件、以完成全部作业的总时间最短为目标函数的集装箱甩挂运输模型.通过算例分析,算出传统集装箱运输与集装箱甩挂运输的车辆等待时间,验证了集装箱甩挂运输模型的可操作性.     

Reverberation time lags in the high luminosity quasar PG 1247+267

Virial estimates of the black hole mass in the center of AGNs, derived from single-epoch observations of luminosity and emission line widths, are now available for several thousands of objects at all redshifts and luminosities, so that studies of the cosmological evolution of the AGN mass function are becoming possible. These estimates are based on the empirical luminosity-size relation measured through reverberation mapping at low redshifts and luminosities. For this reason the spectrophotometric monitoring of 4 luminous quasars was started in 2003, with the 1.8 m telescope of the Asiago Observatory. To measure the reverberation time lag we adopt a method, recently introduced by Zu et al. (2011), which takes advantage of the available statistical information on variability autocorrelation and makes simple assumptions on the continuum-emission line transfer function. We present the estimate of the broad line region size for the quasar PG 1247+267, which is the most luminous object with reverberation measures to date. Virial products computed for C iv and C iii] emission lines provide consistent results. A possible flattening of the size-luminosity relation for C iv at high luminosity is suggested.     

装备时延校准及监控技术研究CSCD

装备时延校准误差是靶场测控系统中事件记录和交会定位的重要误差因素,其精确校准是实现装备时间同步的关键技术。针对装备时延问题展开研究,提出了一种物理含义清晰、易于测量的装备时延定义,实现了离散站点装备时延校准,验证了基于改进型B码的装备时延校准监控的有效性。试验结果表明,时延校准的精度达到了十微秒量级。     

基于空心碳球的超黑涂层的制备与性能研究

针对空间光学系统中的杂散光抑制难题,设计并制备了基于空心碳球(HCS)的超黑涂层。对涂层的颜基比进行优化,发现在最佳颜基比1∶2的条件下,可获得高达0.983的太阳吸收比,结合力等级为2级,符合应用要求。研究表明:在涂层成膜过程中,黏合剂并未进入HCS中空部分,保留的亚波长小孔可有效降低涂层表观折射率,从而降低涂层在太阳波段上的反射率;HSC团聚形成的颗粒有助于涂层形成微米级陷光结构,进一步提高涂层的太阳吸收比。     

基于威布尔分布的CFM56-5B发动机风扇润滑间隔调整方法

分析了发动机产生振动的原因,得出风扇叶片润滑是降低发动机振动水平的最有效方法;基于运行数据使用Minitab工具建模,获得润滑后高振动事件的威布尔分布函数,并得到高振动事件概率,结合安全、成本因素等得出最优润滑间隔;通过机队实践,证明了该方法的有效性。     

B737-300飞机自动增压失效故障分析

增压系统的可靠工作对保障机上人员的生命安全至关重要,为迅速准确地确定增压系统故障,提高航线的排故效率,针对B737-300飞机自动增压系统失效的故障,介绍了故障树的建立依据和方法,并对飞机增压控制系统可靠性进行定性分析和定量分析,该方法在实际航线排故中已得到了初步验证,对提高增压系统排故效率具有重要的参考价值.