某型机载电子设备无失效数据可靠性研究

针对寿命试验过程中未出现失效样本,传统的可靠性分析方法不适用于分析该类产品可靠性的情况,以某型机载电子设备的无失效数据可靠性分析为例,采用贝叶斯无失效数据可靠性评估方法,并综合考虑失效率上限分析其可靠性水平。该方法的预测结果与试验数据相符,在一定置信水平下具有较高的预测精度。     

美军军事通信卫星发展趋势分析及启示

文章讨论了美军先进的军事卫星通信系统,分析归纳了美军卫星通信的特点与发展趋势,并针对我国军事通信卫星发展现状阐述了需要解决的关键技术问题及发展思路。     

美国海军靶船发展研究

美国海军海上打靶训练是演习的重要训练科目,可以测试火炮、导弹、火控雷达的精确性、毁伤威力和作战性能,检验舰艇作战人员武器操控能力和战斗训练水平.本文从美国海军靶船的发展历史、分类、组织管理几个方面进行介绍,并分析其发展特点,为我海军靶船发展提供借鉴.     

H ∞ parameter identification and H 2 feedback control synthesizing for inflight aircraft icing

Aircraft icing accident happens frequently. Researchers try to find new ways to solve this problem. The study is facing the direction of intelligent inspection and control system. Previous studies focused on the principle of aircraft icing and its effects on flight performance. The onboard icing detection equipment can only give the qualitative icing information, but cannot effectively describe how serious the consequences would be. If the icing detection equipment fails, it will cause a serious threat to flight safety. This paper reviews the smart icing system and its fundamental principle. Then based on H∞ theory, an aircraft icing parameter identification method is introduced, and its feasibility is verified by simulation results. Moreover, this method can work normally under noise interference and measurement error. Icing parameter identification method can also test part of aircraft’s stability or control derivatives which would be changed obviously after aircraft icing. Classified by neural networks, the stability or control derivatives’ variation can be mapped to ice parameters’ variation that reflects the severity of aircraft icing. Then H2 state feedback control is designed originally to suppress the impact of noise interference, so aircraft can keep steady after it is iced. Seeing from simulation result of the whole system, it is clear that the system can effectively detect icing parameters and by using feedback control system, it can ensure the safety of aircraft in the flight envelope.     

军用电控汽车故障自诊断系统开发设想

从故障诊断电路和诊断程序、故障诊断标准、网络通讯协议等方面提出了开发研制军用电控汽车故障自诊断系统的设想,对相关内容进行了详细地论述.     

军用电站的电磁屏蔽技术应用

对军用电站的电磁屏蔽设计进行了某些探讨,分析了电站在电磁屏蔽设计中应该注意的关键因素和相应的一些解决办法,为电站屏蔽设计提供一些设计思路。     

64m双幅混凝土简支箱梁造桥机设计

温福客运专线白马河特大桥双幅64m混凝土简支箱梁，共重3200t，采用造桥机一次架设。造桥机的设计采用拆装式军用梁，通过对总体布置和混凝土节段箱梁支承方式的方案比选，确定总体的设计方案，并对各分项设计、施工步骤和关健技术问题进行介绍。     

美国航母飞行甲板演变及设计思想研究

飞行甲板是航母舰载机起降、调运、保障、布列最重要的作业场所,其设计工作在航母总体设计中占有重要地位,很大程度上决定了舰载机出动回收保障能力和航母综合作战效能.本文针对美国海军二战后至今研制的5型航母,分析其飞行甲板布局演变过程,梳理总结美国航母飞行甲板设计思想和启示.     

基于可达性指标的航空货运网络布局优化研究

以网络可达性和利用率最大为目标,建立货机班次分配与货物运输路径选择的多目标双层优化模型,针对我国基于审批方式为各航线分配航班的实际情况,通过调整货机班次优化航空货运网络布局.以20个机场组成的航空货运网络为例,设计NSGAII算法求解模型.结果表明:北京、上海、广州、深圳之间的航段将获得1/4的货机班次,他们是航空货运的枢纽机场;当决策者偏好网络可达性时,更多货机班次将被分配到大型机场间的航段上,当决策者偏好网络利用率时,货机班次在航段上的分配较均匀;随着货机班次在航段上由集中趋向分散,网络可达性降低而利用率提高;减少货机班次会降低网络可达性,增加货机班次会降低网络的利用率.     

‘Each flight is different’: Carbon emissions of selected flights in three geographical markets

Air travel is considered the biggest individual climate sin. Avoiding flying, however, seems impossible. In this paper we argue that the flight a passenger chooses can be significant. For this purpose we compared the carbon emissions of selected flights in three geographical markets. We found tremendous differences in the environmental performance of individual flights. Furthermore, we also found that flying with the most modern aircraft or flying non-stop represents, in many cases, the least polluting option. Nevertheless, we were able to show that there are exceptions to this rule. Based on our results, we provide recommendations to the industry and for further research.