片间综合化互连时间触发通信调度方法

未来先进的分布式综合化航空电子系统需要实现跨越计算体系结构的信息综合,对微小型智能器件间的综合化互连提出要求。通过构建一种具有开放式接口的芯片间综合化互连结构,提出一种相应的时间触发（TT）通信调度方法。首先建立片间综合化互连模型和时间触发流量传输模型,给出负载均衡的选径方法;随后依据传输路径中各级节点各流量的发送时间偏移量计算流量传输的等待时间可行值,利用遗传算法优化调整各芯片发送端口的调度表相位,更新各流量在发送端口的时间偏移量,缩短最坏情况下的最大等待时间,得到具有全局优化意义的时间触发调度表。与使用Yices等SMT形式化求解器的TT调度表生成方法相比,本方法不会出现长时间不停机而无法判定的问题,且不论对于对称或非对称结构,案例研究表明本方法的可调度规模至少增加30%。此外,以流量传输等待时间占周期的比例作为归一化的传输延迟度量,与既有的基于特征任务的调度方法相比,案例研究表明本方法得到的传输延迟最多仅为后者的2%。     

大数据在航空系统的研究现状与发展趋势

针对大数据在航空系统中的应用问题,阐述了学术界与航空工业界在航空大数据采集传输、分析技术及可视化等方面的研究现状。提出了航空大数据平台基础架构,对目前推出的几款航空大数据分析平台结合优化运营、优化维护、降低成本、降低风险等方面的需求进行了评述。指出大数据在航空系统中的应用还存在着理念、方法、技术、人等方面的挑战,并相应地提出大数据组织专门化、处理方法混合化、分析平台柔性化及跨界合作深入化等发展趋势。     

基于鲁棒H_∞控制策略的Hexapod平台低频微振动隔离设计

文章采用一种基于混合灵敏度的鲁棒H_∞控制策略来提高音圈电机驱动的柔性Hexapod平台隔振系统的低频特性;并利用一种基于非光滑优化算法的定结构解算方法快速求解得到低阶稳定的控制器,以解决传统解算方法中高阶复杂控制器难以实现的问题。通过仿真与试验进行频域和时域的验证分析,结果表明:所提出的振动隔离控制策略有效地降低了系统频响曲线的转折频率,提高了低频段的振动衰减率,使柔性Hexapod平台隔振系统的低频隔振效果显著提高。     

星载平面可展天线支撑桁架的结构效率优化

针对折展结构性能存在多指标且这些指标之间又相互制约的特点,把结构效率引入到可展结构的优化设计中,应用多因素正交试验法对一种空间可展开平板天线支撑桁架的优化问题进行了研究。对其关键几何设计参数进行了分析,建立了桁架结构的优化数学模型,以结构效率最大化作为优化目标,对可展桁架进行了结构优化,得到了支撑桁架各杆件的设计参数。结果表明:结构效率综合考虑了质量和刚度的影响,使结构质量和刚度同时得到优化;长宽比(l/w)是影响可展桁架结构性能的主要因素,对不同优化目标产生影响的次要因素有所不同;截面积对结构效率影响不显著(置信度p=90%),在相同杆长参数配置下,等截面可展桁架的结构效率仅次于变截面方案,但工程经济性最佳。该研究方法有助于在概念设计阶段从系统设计的角度进行空间桁架结构的快速设计与优化。     

基于内模原理的复杂挠性卫星姿态控制研究

首先对具有运动挠性附件的航天器的姿态动力学模型进行了简要讨论和分析,证明了对于受步进扰动的复杂挠性卫星系统,采用输出反馈PD控制仅能得到一致有界稳定的结论。为了获得闭环系统的渐近稳定性能,进一步构造了具有内模补偿的PD控制系统,并且根据Lyapunov理论给出了严格证明。基于美国GOES 8号静止轨道气象卫星公布的动力学参数,对PD控制及含有内模补偿的PD控制两类控制器进行了仿真对比,以校验所设计控制系统的有效性。最后,进行了总结并提出进一步的研究设想。     

Fractional Pfaff-Birkhoff Principle and Birkhoff′s Equations in Terms of Riesz Fractional Derivatives

The dynamical and physical behavior of a complex system can be more accurately described by using the fractional model.With the successful use of fractional calculus in many areas of science and engineering,it is necessary to extend the classical theories and methods of analytical mechanics to the fractional dynamic system.Birkhoffian mechanics is a natural generalization of Hamiltonian mechanics,and its core is the Pfaff-Birkhoff principle and Birkhoff′s equations.The study on the Birkhoffian mechanics is an important developmental direction of modern analytical mechanics.Here,the fractional Pfaff-Birkhoff variational problem is presented and studied.The definitions of fractional derivatives,the formulae for integration by parts and some other preliminaries are firstly given.Secondly,the fractional Pfaff-Birkhoff principle and the fractional Birkhoff′s equations in terms of RieszRiemann-Liouville fractional derivatives and Riesz-Caputo fractional derivatives are presented respectively.Finally,an example is given to illustrate the application of the results.     

Influence of lunar topography on simulated surface temperature

The surface temperature of the Moon is one of the essential parameters for the lunar exploration, especially to evaluate the Moon thermophysical features. The distribution of the temperature is heavily influenced by the Moon topography, which, however, is rarely studied in the state-of-art surface temperature models. Therefore, this paper takes the Moon topography into account to improve the surface temperature model, Racca model. The main parameters, such as slopes along the longitude and latitude directions, are estimated with the topography data from Chang’E-1 satellite and the Horn algorithm. Then the effective solar illumination model is then constructed with the slopes and the relative position to the subsolar point. Finally, the temperature distribution over the Moon surface is obtained with the effective illumination model and the improved Racca model. The results indicate that the distribution of the temperature is very sensitive to the fluctuation of the Moon surface. The change of the surface temperature is up to 150 K in some places compared to the result without considering the topography. In addition, the variation of the surface temperature increases with the distance from the subsolar point and the elevation, along both latitude and longitude directions. Furthermore, the simulated surface temperature coincides well with the brightness temperature in 37 GHz observed by the microwave sounder onboard Chang’E-2 satellite. The corresponded emissivity map not only eliminates the influence of the topography, but also hints the inherent properties of the lunar regolith just below the surface. Last but not the least, the distribution of the permanently shadowed regions (PSRs) in the lunar pole area is also evaluated with the simulated surface temperature result.     

Determination of land surface temperature using precipitable water based Split-Window and Artificial Neural Network in Turkey

Land surface temperature (LST) calculation utilizing satellite thermal images is very difficult due to the great temporal variance of atmospheric water vapor in the atmosphere which strongly affects the thermal radiance incoming to satellite sensors. In this study, Split-Window (SW) and Radial Basis Function (RBF) methods were utilized for prediction of LST using precipitable water for Turkey. Coll 94 Split-Window algorithm was modified using regional precipitable water values estimated from upper-air Radiosond observations for the years 1990–2007 and Local Split-Window (LSW) algorithms were generated for the study area. Using local algorithms and Advanced Very High Resolution Radiometer (AVHRR) data, monthly mean daily sum LST values were calculated. In RBF method latitude, longitude, altitude, surface emissivity, sun shine duration and precipitable water values were used as input variables of the structure. Correlation coefficients between estimated and measured LST values were obtained as 99.23% (for RBF) and 94.48% (for LSW) at 00:00 UTC and 92.77% (for RBF) and 89.98% (for LSW) at 12:00 UTC. These meaningful statistical results suggest that RBF and LSW methods could be used for LST calculation.     

一种提高我国空间站中继测控覆盖率的方法

根据中继卫星的定点位置,对我国中继卫星-空间站的几何覆盖率进行了分析,并对提高空间站中继测控覆盖率的途径进行了研究,提出了一种采用不同舱段的2副中继天线融合使用,并通过调整天线安装布局提高中继测控覆盖率的方法。经理论分析和仿真验证,该方法能够有效地提高空间站中继测控覆盖率,可为我国空间站中继天线的安装布局设计提供参考。     

四轴飞行器姿态监控系统设计

设计了一套四轴飞行器上位机监控系统。针对准确掌握四轴飞行器的实时姿态、位置等信息和对四轴飞行器进行精准控制两大核心问题,开发了由上位机实现四轴飞行器姿态数据采集、通信及控制等功能的监控系统。监控系统良好的功能设计和友好的人机界面使得用户能够准确掌握飞行器的飞行信息,从而能够更精准地控制四轴飞行器飞行姿态。实验验证,监控系统简单实用,性能稳定,精度高,使整个飞行系统抗干扰能力强,鲁棒性、稳定性好。