一种基于粗糙K-均值的椭球基函数神经网络

改进了一种椭球基函数神经网络,它与经典椭球单元神经网络的结构不同,而与径向基函数神经网络结构类似,即它有一个隐含层,并且隐层单元采用椭球基函数,区别于RBF网络的高斯函数。本文采用粗糙K-均值方法求取椭球函数的中心,并给出了该方法中确定初始阈值的步骤。这种改进方法不但使对输入空间的划分局部作用,而且划分区域封闭有界。因此,改进的神经网络具有较好的函数逼近能力和模式识别能力。仿真实验验证了该椭球基函数神经网络的正确性和有效性。     

试论科技论文的语言特点

阐述了科技论文在现代社会中的重要地位和作用，着重探讨科技论文的语言特点。在科技论文中使用多语系语言，且除了使用自然语言符号系统以外，同时大量使用超自然语言符号系统。科技论文要求语言简明、精确，逻辑性强，并严格遵守有关的规范和标准；在语法上则多采用存在句、泛指句和析使句，常用第三人称。     

攻角传感器的热失效分析与设计方案改进

根据压差归零式攻角传感器的工作原理、结构及工作条件，结合实际经验，分析了该传感器的主要失效因素，并重点分析了热失效问题；探讨了飞行中传感器探头加热器与环境之间的热交换情况。     

航天航空中急性缺氧条件下功效改变的研究

受试者为84名男性青年和实验工作人员,在低压舱1500、2500、3000、4000、5000和6000米高度上停留60分钟。每次实验一个高度,总共133人次。实验中,记录了数字记忆、听觉警觉和跟踪操作等多项功效指标。应用统计和模型方法对结果进行了分析,并试用模糊集理论对五种基本功效进行综合评定,得到了急性缺氧下功效改变有意义的结果。这些结果可为飞行员执行飞行任务,航天员在船舱内或穿着航天服在舱外执行任务及制订医学保证方案提供了科学依据。     

Σ-演算的范畴模型

Σ-演算是并发演算CC的子理论,集中体现CC中的并行运算部分的特征。本文将并发通信系统看作是由状态加变换构成的动态系统,建立了Σ-演算的范畴模型(Categorical ModeI),其基本思想是:把Σ-演算中的公式对应于范畴构造中的对象(Objects),Σ-演算中的推演对应于范畴中的态射(Morphisms),从而通过Σ-演算的结构操作语义自然地得到一种范畴结构。这种方法可以推广到其它并发理论之中,例如网论和逻辑方法(如线性逻辑Linear Logic),从而范畴论可以作为描述并发、通信和非确定性行为的统一的形式化框架。     

多尺度子域基函数矩量法解的稳定性与迭代法

通过对几个具体实例的计算，证实了在电磁场边值问题的矩量法求解过程中，选用不同的基函数其解的数值稳定性会有很大的差别。从而有可能选择一种数值稳定性比较好的基函数来进行矩量法求解。另一方面，提出了选用多尺度子域基函数，并通过多次迭代来提高矩量法解的精度的算法。实例计算表明，该算法不仅可以有效地降低系数矩阵的条件数，而且还降低了对计算机内存容量的要求，是一种有效的、稳定的算法     

超静超稳卫星碰振动力学建模

针对分离式卫星载荷模块(PM)受到扰动时可能与服务模块(SM)发生碰撞的问题，综合音圈电机反电动势(back-EMF)和柔性线缆动力学的效应，基于牛顿欧拉法建立了分离式卫星(DFP)载荷模块动力学模型。基于Hertz接触理论，推导了分离式卫星碰撞过程中连续接触力模型，并分析了碰撞过程中产生的接触力对载荷模块指向精度和指向稳定度的影响。数值仿真结果表明，碰撞使得载荷模块指向精度和指向稳定度下降5个数量级，碰撞后载荷模块可再次恢复到超静超稳工作状态，恢复时间超过1400 s。本文建立的碰撞模型对研究分离式卫星碰撞规避和碰撞控制具有重要意义。     

Methane pyrolysis in preparation of pyrolytic carbon: Thermodynamic and kinetic analysis by density functional theory

The density functional theory has been successfully applied in analyzing pyrolytic carbon deposition by methane pyrolysis from the view of thermodynamics and kinetics based on a total number of 39 elementary reactions. M06-2X/def2-TZVP level was employed to optimize species structures and locate the transition states. The enthalpy changes and Gibbs free energy changes of all the reactions in the temperature range of 298.15–1800 K were derived with optimized species. Results show that the reacting temperature should be above 1200 K based on the equilibrium constant analysis, which is consistent with the typical reaction temperature adopted in experiments. Potential energy surface profiles report that radical attacking reactions have lower energy barriers than those direct decomposition reactions, especially hydrogen radical attacking reactions. The energy barriers of the first steps, dehydrogenations of methane and ethylene, are 272.4 kJ·mol⁻¹ and 288.9 kJ·mol⁻¹ at 1200 K, which are very close to the experimental activation energy for methane pyrolysis. The most favorable decomposition reaction path is the path of hydrogen radical attacking reactions. The highest energy barrier of the path at 1200 K is 185.7 kJ·mol⁻¹ presented by the C–H bond breaking in ethynyl attacked by hydrogen radical.     

Quantitative assessment and visualization of flight risk induced by coupled multi-factor under icing conditions

Aircraft icing has been proven to be one of the most serious threats to flight safety. During the analysis of flight risk under icing conditions, quantitative assessment and visualization of flight risk are quite essential as they provide safe manipulation strategies in intricate conditions. However, they are rarely studied. Since the icing flight accidents are the result of the coupling of multiple unfavorable factors, in present study, we have proposed a method to quantitatively assess flight risk induced by multi-factor coupling under icing conditions by Monte-Carlo simulation and multivariate extreme value theory. The results demonstrate that the flight risk probability increases with the rise of unfavorable factors. Besides, a flight risk visualization method named flight safety window has been presented to build the flight risk distribution cloud maps in different complex conditions. The cloud maps show that the icing would give rise to atrophy of the safety scope, and the consequence would be even more severe when coupled with other more unfavorable factors. The proposed methods in this study would be useful in flight risk analysis under icing conditions and can enhance the pilot's situational awareness in selecting correct strategies within the safety zone to avoid unsafe manipulation.     

电动式磁悬浮动量球电磁场耦合分析

本文针对电动式磁悬浮动量球(Electrodynamic suspension reaction sphere, EDSRS)的电磁场耦合进行分析，采用定子绕组的感应电动势评判耦合强度，提出了耦合强度评判指标，作为EDSRS的结构设计约束，以降低电磁场耦合的影响。首先，结合EDSRS的具体结构特点，对多定子之间的电磁场耦合问题进行分析，采用定子电磁场在另一个定子绕组中产生的感应电动势评判耦合强度。然后，对感应电动势产生规律进行分析，提出了耦合强度评判指标，并基于所提评判指标，建立了耦合约束验证流程，作为EDSRS的结构设计约束，最后，通过有限元仿真和实验验证了上述电磁场耦合分析。