A320飞机滑行跑偏故障原理浅析

通过对一起空客A320系列飞机在低速滑行时出现跑偏故障的介绍,从故障现象、系统原理、排故过程等方面对滑行跑偏故障进行了分析和总结。     

《电子商务概论》课程体系改革探索

分析了＂电子商务概论＂的课程性质,指出了其在现阶段课程教学中存在的问题,结合自身实践教学经历,从课程理论内容到实践教学内容出发,设计了一套集＂课内＋课外＂,＂校内＋校外＂的课程教学体系,为电子商务概论的课程建设提供参考。     

自适应滑模控制在飞机前轮转向中的应用

前轮操纵系统是大型飞机实现地面滑行机动和按预定轨迹起降控制的关键系统之一。针对轮胎转向时复杂的负载特性以及电液伺服系统自身存在的非线性和参数不确定性的特点,基于滑模控制理论,结合Lyapunov稳定性理论,给出了飞机前轮转向滑模控制方案,并进行了数字仿真。结果表明,所设计的滑模控制器具有鲁棒性强、结构简单、易于实现的优点。     

Human engineering for the space station

Human factor engineering standards and considerations for the International Space Station are reviewed. Factors considered for laboratory and habitation modules, workstations, visual displays, and EVA worksites are discussed.     

大型航天器SGCMG系统基于模糊决策的操纵律设计研究

作为航天器制导、导航和控制系统的执行部件,单框架控制力矩陀螺是较为理想的大型航天器姿控系统的选择,但是单框架控制力矩陀螺系统（ＳＧＣＭＧ）存在严重的奇异现象,增加了操纵律的设计与开发的难度。本文对ＳＧＣＭＧ系统的奇异性进行了分析,利用模糊决策的思想确定了奇异测度,根据奇异测度梯度搜索法设计了基于模糊决策的ＳＧＣＭＧ系统操纵律。仿真试验表明该方法有效地保证了系统能够回避可避的奇异状态,为大型航天器操纵律设计提供了新的思路。     

某型组合导航系统电动舵机抖动故障分析

针对某型组合导航系统总体测试时发现的电动舵机抖动故障,分析了该组合导航系统A3板再平衡回路的组成及工作原理,建立故障树并开展故障排查,明确了故障原因。通过制定改进措施,可以有效降低组合导航系统故障率,提高产品可靠性。     

自导段航向稳定性研究

针对飞行试验中出现的自导段航向振荡发散现象,通过理论分析、数学仿真和半实物仿真试验,找到了稳定性不好的原因,采取了改善措施,获得了满意的飞行试验结果,自导段航向稳定性问题得到圆满解决.     

数字式飞机起落架转弯控制器设计

针对某型飞机起落架转弯控制系统,本文设计了一种以DSP和双口RAM为核心的双余度数字式控制器.控制器采用硬件冗余的方法搭建双通道热备份系统,制定了余度管理策略.借助自检测和比较监控技术实现一次故障工作、两次故障安全的目标.运用马尔可夫过程建立了系统的可靠度模型,利用MATLAB求解可靠度模型的微分方程组,并对系统的可靠度进行了仿真分析.     

42CrMo汽车转向节臂的热处理工艺改进

通过汽车转向节臂断裂后的硬度检查及金相组织分析,对该零件的热处理工艺进行探讨,确定合理的热处理工艺参数,有效的解决生产中的实际问题.     

A Combined Programmed and Adaptive Null Steering Technique

The described method of antenna null steering makes use of calibrated and stored weight distributions for each solid angle increment of a radar search volume. Based upon direction measurement to an interference source, the appropriate weight distributions are calculated for each relative antenna position. In addition to the programmed part an adaptive inner loop is included for fine null adjustment. The major parameters and characteristics of the null steering technique are studied and evaluated through computer simulation programs.     

Electronically Variable Time-Delay Network for Broad-Band Phased-Array Steering

This paper describes an electronically variable time-elay network that has been developed specffically for time-delay steering of a phased-array antenna. The network consists of microwave dispersive delay lines and two broad-band mixers; its delay is a function of the mixers' local oscillator frequency. The particularly advantageous feature of this network is that its phase is invariant with delay. It can, therefore, be used on a subarray basis, and at IF, without affecting the phase progression across the array. Alternative techniques, such as electron-beam delay lines and digitally switched line lengths, require external phase correction. A breadboard model of the network has been built and tested. Low-loss folded-tape meader lines provide the dispersive delay. The center frequency of the model is 3 GHz; it handles an instantaneous bandwidth of 300 MHz. Delay variation of 25 ns is provided. The spurious responses of the network are 30 dB down.     

稳中求胜 发展民族机床产业——访北京航空制造工程研究所数字化制造与柔性装配技术研究室主任刘华东

中国机床工业经过多年发展,已经积累了一定的产业和技术基础,但却仍然存在一定的问题和差距。北京航空制造工程研究所数字化制造与柔性装配技术研究室主任刘华东曾在陕飞主管飞机装配工作,并兼任航空数控机床协会的专家,集用户、专家、供应商的身份于一身,他对中国数控机床产业发展的看法应该是独特的。为此,本刊特别采访了刘华东主任,请他就我国数控机床的发展进行了深入的分析。     

我们会回来——美国航空公司亚太区副总裁采访

美国航空公司(American Airlines)曾经是美国也是世界上最大的航空公司,2011年11月29日向美国南纽约区破产法庭提交了自愿重组申请。这是一场有备而来的博奕,申请破产时的美国航空母公司还有41亿美元现金,远高于美达美航破产时的15亿美元和美联航破产时的8亿美元。     

The Effect of Random Steering Vector Errors in the Applebaum Adaptive Array

The effect of random errors in the steering vector of an Applebaum adaptive array is examined. Each component of the steering vector is assumed to have a random error component uncorrelated between elements. The array output signal-to-interferenceplus-noise ratio (SINR) is computed as a function of the error variance. It is shown that the array output SINR becomes more sensitive to steering vector errors as more elements are added to the array and as the received desired signal power becomes larger. The variance of the steering vector error that may be tolerated depends on the required desired signal dynamic range. The larger the dynamic range that must be accommodated, the smaller the error variance must be.