失去润滑的高速滚动轴承工作游隙的分析

分析了某武装直升机传动系统在失去润滑状态下其高速滚动轴承工作游隙的变化情况, 推导出考虑构件弹性时轴承游隙变化量的计算公式, 并以实例验算。为合理选择滚动轴承游隙值, 提高轴承系统寿命乃至整个传动系统生存力提供依据      

深空探测多天线组阵的增益损失研究

为定量分析上行天线组阵增益损失的影响因素,提出一种通过建立数学模型分析合成损耗的估计方法.首先基于天线原理和电磁波传输理论建立了天线组阵上行链路信号的数学模型,以统计学理论对数学模型进行分析,得到了影响上行链路信号的若干因素.通过分析得出,深空探测信号在远距离传输中因大气相位扰动引起的误差是造成天线组阵增益损失的最主要因素.再通过对大气相位扰动误差的进一步分析,构建S频段和X频段下大气相位扰动的空间自相关模型和时间自相关模型,得到组阵基线长度和工作仰角同合成损耗的关系.经过对各误差源的分析可知,在目前的技术水平下,能够满足上行天线组阵工程应用的精度要求.     

Performance of Sidelobe Blanking Systems

Sidelobe blanking systems are useful in preventing acquisition of strong targets in the antenna sidelobes and also in rejecting pulsed interference originating in the sidelobes. The analysis of a common two-channel system is presented in which the relationship between the probability of main-lobe detection and the probability of sidelobe detection are given in terms of false-alarm probability, signal-to-noise ratio, and the ratio of sidelobe levels of the two channels. The numerical results given provide a basis for the selection of the sidelobe blanking channel antenna gain and threshold levels.     

Calculating the Effect of Uneven Terrain on Glide Path Signals

A method for calculating the bends in the glide slope due to uneven terrain is presented. A computer program written for the purpose enables the calculation of the difference in depth of modulation (DDM) at any point, taking into account the effect of uneven terrain. Results are presented for a hypothetical case of a hill in front of the runway. The program enables us to predict the glide slope bends due to irregular terrain, so that proper selection of glide slope antenna location can be made.     

Analysis and Design of Antennas for Air Traffic Collision Avoidance Systems

The analysis and design procedure of an antenna for a CW Doppler radar system being developed for pilot warning of midair collision hazards is presented. The antenna consists of two vertical arrays of half-wavelength dipoles mounted near a circular conducting cylinder. Each vertical array is composed of three vertical dipoles. Each array provides relatively uniform illumination (2-3 dB) in the forward 180 angular segment of the horizontal plane and approximately + 10-150 coverage in the vertical plane. The antenna could be used in a two-mode operation, either in a standard monopulse radar system (sum and difference amplitude patterns) or in a system where amplitude and phase are the measurable quantities.     

基于人工免疫的直升机传动系统在线异常监测方法

 针对直升机在线监测时难以提取状态特征的问题，提出一种适用于直升机传动系统在线状态监测方法。该方法基于生物免疫系统反面选择机理，利用改进型反面选择算法并结合人工神经网络进行监测。该方法能有效地提取直升机传动系统的状态特征，并结合直升机传动系统的实际情况准确得出状态异常度。在线监测实例结果表明，该方法能较准确监测出直升机传动系统的异常状态，验证了该方法具有较好的在线性、准确性及鲁棒性。     

Cross Polarization in Radomes: A Program for Its Computation

A study is made of transmission by radomes, with particular reference to cross polarization, and of the consequent radiation patterns of the radome with its aerial for both linear and circular polarizations. The work is embodied in a computer program which considers a scanner of specifiable size, position, and power distribution at different orientations inside a multilayer radome of given dimensions, class of shape, and construction in terms of the number and properties of its layers. Initially, rays are traced from points on the scanner, and details of their paths and propagation are presented in tables of preliminary results; later, diffraction theory is used. Polar diagrams of cross polarization, of main beam, etc., are presented in final tables for the system. Nearly all the parameters are specifiable, and so the program has reasonably general applicability, and it can also assess the effects of bandwidth, tapering of layer thickness, complex permittivity, and other parameters of the system.     

微带天线的多频特性

引言 微带天线由于具有一系列独特的优点,正在受到人们越来越多的重视,可以预计,在不远的将来,微带天线将在很广泛的应用场合取代人们已应用了多年的一大类天线。 微带天线固有的一个重要特性——多频特性,即一个微带天线可以在离散的多个频率点上工作的特性,至今尚未被人们所充分认识、研究和利用。本文初步研究了微带天线的多频特性（对VSWR而言）,包括多频的观测、实验和理论分析。     

On the Perfomance of Air Traffic Control Radar Beacon System

The sidelobe suppression and improved sidelobe suppression mode performance of terminal and enroute air traffic control radar beacon systems using the existing antenna and a typical improved antenna in the presence of perfectly dielectric flat ground are investigated theoretically. Necessary analytical expressions for various quantities characterizing the system performance have been derived. A general purpose computer program has been developed for the computation and tabulation of these quantities as functions of the elevation angle of the observation point and for different combinations of heights of the directional and omnidirectional antennas of the beacon. Although the discussions given here apply to some specific antenna configurations, the theoretical method developed has more general application in evaluating quantitatively the performance of the beacon system in a given situation.     

基于光纤光栅变形光谱的疲劳裂纹扩展监测方法

为研究金属疲劳裂纹扩展的在线监测技术,基于改进传输矩阵的光谱模拟方法,建立反映光纤布拉格光栅（FBG）光谱变形机理的裂纹扩展在线监测方法。研制了疲劳裂纹扩展在线监测系统平台,提出基于平移不变量小波法的试验光谱去噪方法,解决试验光谱信号中非连续与快速变化点难以平滑的问题;提出仅与裂纹扩展状态相关的FBG光谱面积参数,克服了光谱中心波长、光谱带宽等传统特征参数仅适用于恒定外载与恒定温度或对裂纹不敏感的局限性,给出基于光谱面积曲线拐点的裂纹扩展状态判定依据。     

天线窗材料热透波特性风洞测试方法

高超声速飞行器天线窗材料在等离子体包覆条件下的热响应和热透波特性测试,是分析天线窗材料特性、研究电磁波在等离子体和天线窗中传输特性的基础。针对等离子体和天线窗中电磁波传输特性,采用矢量网络分析仪和标准增益天线组成的电磁波传输测试系统,获得了一定频率的电磁波经过等离子体和高温天线窗之后的衰减;针对高温天线窗自身热响应特性和电磁波在其中的传输特性,研究了天线窗材料在一定热流作用下的温度分布和烧蚀特性,测试了烧蚀后处于高温状态且无等离子体覆盖的天线窗对电磁波的影响,分析了天线窗高温透波特性与常温透波特性的差异。所建立的方法,为在地面等离子体风洞中开展天线窗热透波特性研究、分析天线窗和等离子体耦合作用对电磁波传输特性的影响建立了基础。     

雷达罩的综合优化设计

在分析对比现有的雷达罩设计方法基础上，针对某型直升机机栽雷达罩，研究了雷达罩设计过程中的基本问题、关键技术和综合优化设计方法，运用三维射线追踪法进行了计算机辅助设计，给出了布设防雷击部件的经验公式，讨论了吸波材料选择与喷涂的基本准则。电测结果表明：加罩后的功率传输系数、反射瓣、雷达辐射特性等指标的实测数据与计算值符合较好，满足了设计要求。     

DIMA架构下飞机全电刹车系统故障传播行为分析与评估

在DIMA平台开放性体系架构的背景下,飞机航电与机电等系统功能逐渐渗透融合,面向DIMA架构的全电刹车系统是未来飞机刹车系统的主流设计趋势,但目前尚未形成针对DIMA架构下全电刹车系统的故障传播行为分析与评估方法。针对上述问题,首先结合DIMA架构特征和全电刹车相关标准,分析面向DIMA架构下的全电刹车系统分层架构,在此基础上构建全电刹车系统任务-功能-资源层次模型。其次,考虑到DIMA平台资源共享的特点,结合系统层次模型开展系统耦合关联分析,引入Floyd算法计算间接耦合矩阵以及路由矩阵,通过构造失效严重程度矩阵量化系统关联耦合度,建立系统故障传播结构模型,综合考虑故障路径传播概率和系统边缘介数,构建DIMA架构下全电刹车系统故障传播强度模型,以识别系统故障传播关键路径,完成故障传播行为分析与评估。最后通过实例分析,以验证所提方法的正确性与合理性。     

Strapdown inertial measurement units for motion compensation forsynthetic aperture radars

It is shown that synthetic-aperture radar (SAR) motion can be compensated by using an antenna-mounted strapdown inertial measurement unit (IMU) as the motion sensing system, but sensor and system errors affect SAR image quality. A strapdown IMU consists of three accelerator channels and three gyro channels. Strapdown IMU errors include gyro-scale and accelerometer-scale factor and bias errors, velocity error, platform tilt, and errors induced by limited inertial sensor bandwidth. The effects of these errors on the SAR image quality are presented in terms of the SAR impulse response. IMU errors that cause low-frequency phase errors (less than one cycle per array time) are categorized in terms of quadratic and cubic phase errors. IMU errors that cause high-frequency phase errors (greater than one cycle per array time) are categorized in terms of the integrated sidelobe ratio and peak sidelobe ratio. A motion compensation system conceptualization is described wherein a strapdown IMU is attached to an antenna and transfer-aligns to the aircraft's master navigator     

A Bound on Processor Gain

In data transmission systems using electromagnetic propagation there is often interest in the antijam capability of the system and the probability that the transmitted signal can be intercepted. It is shown that, neglecting antenna gain, both of these are adequately described by the processor gain. An information theoretic bound is given for the processor gain and the performance of several conventional signaling systems is indicated. Improvement using forward error correction is also investigated.     

行星齿轮传动系统的稳态热分析

行星齿轮传动系统中,各零部件的本体温度和温度场的分布对系统的工作性能和可靠性有重要影响。以直升机的主传动系统中的行星齿轮系统为对象,建立了其发热模型和热传递模型,利用热网络分析法从而得到该系统的稳态温度分布,为行星齿轮传动系统的稳态热分析提供了一个有效的方法,并为行星齿轮系统的瞬态热分析奠定了基础     

Noise factor of receiving system with arbitrary antenna impedancemismatch

The system operating noise factor of a receiving system is modeled for arbitrary impedance mismatch of the antenna to the transmission line feeding the receiver. The effect of this mismatch on the noise factors of the transmission line and the receiver is considered. The stochastic nature of the external noise factor is considered. The amount of mismatch that can be tolerated before the internal system noise factor exceeds the external noise factor is determined. Numerical results are presented for a VHF-FM radio receiving system with an electrically short monopole antenna. It is noted that a large impedance mismatch at the antenna-transmission-line interface of a radio receiving system can cause a significant increase in the system internal noise factor (more than a 50-dB increase for a voltage reflection coefficient of 0.999)     

喷气发动机转速数字控制器优化设计

喷气发动机转速数字控制系统的构成和动态模型如图1所示。数字控制器由微机编程实现。该闭环系统由PID控制器进行串联校正、角度负反馈为位置反馈校正。     

飞行控制系统的输出反馈最优设计

本文在频域范畴内,利用输出反馈方法论述了在二次型性能指标下多变量线性最优调节器的控制问题,通过把多变量系统的前馈解耦控制与最优控制结合起来,得到了最优控制解的频域形式。这种最优控制规律既可使系统的能耗和输出偏差综合最优,具有较好的抗干扰性,又可满足给定的时域性能指标。方法简单,求解方便,便于工程应用。作为例子,文中对某纵向飞行控制系统进行了最优设计。     

应用Fuzzy ISODATA方法选择航空科研项目

 本文将Fuzzy ISODATA方法用于科研项目的选择,并结合中国航空发动机涡轮冷却专业的科研选题实例进行了定量分析。用Fuzzy ISODATA方法将14个备选项目按其对总目标的贡献值划分为3类。结果表明,该方法具有划分合理,结果直观,计算速度快便于对大量项目进行选择的优点。