Wavelength dimensioning for wavelength-routed WDM satellite network

Internet and broadband applications driven by data traffic demand have become key dri-vers for satellite constellations. The key technology to satisfy the high capacity requirements between satellites is optical satellite networks by means of wavelength division multiplexing inter-satellite links (ISLs) with wavelength routing (WDM-OSN). Due to the limited optical amplifier bandwidth onboard the satellite, it is important to minimize the wavelength requirements to provi-sion requests. However, ISLs should be dynamically established and deleted for each satellite according to its visible satellites. Furthermore, different link assignments will result in different topologies, hence yielding different routings and wavelength assignments. Thus, a perfect match model-based link assignment scheme (LAS-PMM) is proposed to design an appropriate topology such that shorter path could be routed and less wavelengths could be assigned for each ISL along the path. Finally, simulation results show that in comparison to the regular Manhattan street net-work (MSN) topology, wavelength requirements and average end-to-end delay based on the topol-ogy generated by LAS-PMM could be reduced by 24.8%and 12.4%, respectively.     

AIRCRAFT CONCEPT EVALUATION AND EFFECTIVENESS-BASED DECISION-MAKING

Based on effectiveness analysis, a novel method is presented for combat aircraft top-hierarchy concept evaluation and decision-making. Applying multi-criterion decision-making （MCDM） and analytic hierarchy process, the new method can help to overcome the limitations of existing evaluation systems and decision-make methods. The proposed method includes the following process~ （1） Establish a multi-criterion and multi-hierarchy evaluation attribute system by introducing combat effectiveness~ （2） Assign weight to the attributes and normalize them; （3） Evaluate and decision-make top-hierarchy aircraft concept based on effectiveness to reach a satisfactory design by comprehensively applying four multi-criterion decision-making methodologies, i.e. grey correlation pro- jection method, weighted summation method, weighted quadrature method and ideal solution decision-making method, while considering the attribute hierarchy system and the logical relations among the attributes. Finally, an example is given to indicate the validity and feasibility of the proposed method.     

基于高斯伪谱法的飞机下降段轨迹优化

以大型运输机为研究对象,进行风干扰下的飞机下降段轨迹优化.通过对飞机下降过程的分析,建立了飞机的运动学模型、油耗模型和大气模型,得出了问题的目标函数和约束.运用高斯伪谱法把最优控制问题转化为非线性规划问题,并用序列二次规划求解非线性规划问题.仿真计算得到飞机最短下降时间的最优轨迹,讨论了不同的成本指数对下降时间和燃油消耗的影响.仿真结果表明,成本指数越大,飞机下降时间越短,燃油消耗越多.     

左、右手媒质间电磁传输特性的对比分析

文章通过重新表述折射率，对比分析了左、右手媒质不同组合情况下，电磁波在媒质界面上的折射特性。通过引入色散关系的时域有限差分法对无限大左手介质板以及线源置于左手媒质覆层内两种模型进行了模拟，模拟结果与分析相符合。分析表明，负折射现象出现在界面两侧媒质类型（LHM／RHM或RHM／LHM）不同的情况下。对于同种类型媒质的情况，左手媒质并不能引起反常的折射现象。LHM引起的反常现象通过与RHM的对比才能得以有效考察。     

"公寓"型LRU可靠性指标的预计法探讨

探讨了“公寓”型LRU可靠性预计的方法，“公寓”型LRU的电子元器件不属于同一系统，因此不能按“串联”型预计，如何预计则应进一步研究，本文提出了预计的3种方法。     

基于主成分的编队级网络对抗效能评估指标体系

分析建立编队级网络对抗评估指标体系的原则,用主成分分析法对指标进行处理,求得7个主成分.根据正交原则将20个指标分配到7个主成分中,赋予每个主成分以实际含义,最终建立了编队级网络对抗效能评估指标体系.     

卫星遥测功率谱分析和调制度测量方法研究

残余载波调制是卫星测控中的常用调制体制。文章从理论上给出了该体制下信号的功率谱密度表达式，得到奇次谐波谱线展宽等结论，并通过仿真和实验进行了验证。利用所得结论讨论了遥测调制度测量方法，提出通过功率谱的2阶边带进行测量可以使结果得到改善。     

基于数值模拟的超塑成形压力—时间曲线计算机辅助设计

确定压力随时间变化的关系曲线对于超塑成形工艺设计非常重要，本文在超塑成形压力计算时引入能量消耗控制策略，提出了一种压力－时间（Ｐ－Ｔ）曲线设计方法即恒能耗率法，实现了基于有际元数值模拟的超塑成形Ｐ－Ｔ曲线计算机辅助设计，文中对有关的压力控制算法及算式进行了较详细的介绍和推导，分别给出了半球壳自由胀形和圆筒形凹模约束成形过程的Ｐ－Ｔ曲线设计计算实例，并对计算结果进行了讨论，本文的研究拓宽了刚粘塑性有     

民用飞机维修目标与要求的指标体系研究

维修目标与要求(MORs)是为了能够并便于对产品进行维修而对航空器设计、维修和保障所提出的目标与要求,是设计、使用、维修、成本、效率等多种因素的综合权衡结果,也是维修工程学要实现的具体要求和指标。本文立足民用飞机,结合自身民机维修经验,从MORs指标确定的风险、过程、指标的分类等方面对MORs及其指标进行了研究。     

基于支持向量机的航空发动机性能衰退指标预测

针对航空发动机性能衰退状态的趋势预测问题,基于非线性支持向量机回归建立了发动机性能衰退指标的预测模型,给出了反映其性能衰退的综合指标。利用该模型对发动机的性能衰退指标进行了预测分析,并与神经网络模型预测结果进行了比较。结果表明:支持向量机回归预测模型能更准确地对发动机的未来状况进行预测。