Pull-In Time and Range of Any Order Generalized PLL

The general pull-in range and pull-in time expressions are derived versus the relevant system parameters and the initial detuning for any order loop with any type of phase detector by the quasistationary approach. Even though the pull-in time expression becomes more accurate as the loop's order becomes larger, it is correct also for second-and third-order loops provided that the initial detuning, supposed large, is approaching the pull-in range value.     

Acquisition Time of Tracking Loops Operating in the Frequency-Search Mode

This paper presents a theory for computing the signal acquisition time of a second-order tracing system operating in the frequency-search mode. In particular, a closed-form expression is obtained which relates the acquisition time to the relevant system parameters, to the initial loop detuning, and to the slope of the ramp that sweeps the voltage-controlled oscillator. Although the theory is only approximate and the resulting formula is exact only in the limit when the initial loop detuning ?F goes to infinity, it has been found that it gives quite accurate results as soon as ?F is some times greater than the equivalent noise bandwidth of the loop.     

错频叶盘结构的概率模态局部化特性分析

以典型压气机叶盘结构为例,提出了实际错频结构的有限元建模方法,并考虑了随机加工误差的影响,定义了一种基于叶片应变能的模态局部化因子,基于ANSYS有限元和Monte Carlo数值计算,定量分析评价了错频叶盘结构固有频率和模态振型局部化的统计特性.研究表明,"错频失谐"会引起显著的振动局部化,叶盘错频设计中需要综合考虑结构的失谐振动局部化和气弹稳定性两方面.      

单轴稳定技术在盘旋跟踪地面目标中的应用

针对小型无人机,设计一种安装于机身左侧下方的单轴光电探测系统来修正视场纵向误差,同时配合无人机的航向控制,对目标进行盘旋跟踪。控制系统在设计过程中采用纵向通道和横向通道解耦、方位失谐量修正和俯仰失谐量修正解耦的控制方式。飞行试验表明,该控制方式能够持续稳定的跟踪地面目标,使地面目标的成像点趋向于光心,达到了盘旋跟踪的预期效果。     

The effect of detuning of the partial frequency of MEMS gyros sensing elements on the amplitude-frequency response

The effect of detuning the partial frequencies of MEMS gyroscopes on its amplitudefrequency response is investigated. The formulated mathematical model allows defining requirements for the tolerances on gyros parameters, which determine the values of gyros partial frequencies, at the design stage of the sensor.     

Reception of pulsed signals by detuned receiver: addenda andcorrections

The parameters of a pulse perturbed by passage through a filter were examined in a variety of cases in a previous paper by the author (ibid., vol.AES-4, p.486-9, May 1968). One case not covered is that of a rectangular pulse passed through a detuned Gaussian filter; that case is presented, as is the case of a swept Gaussian pulse passed through such a filter, which may be dispersive. Corrections are included for two tabular entries in the original paper concerning a Gaussian pulse fed to an ideal bandpass filter when the time-bandwidth product and detuning are large     

Response regimes of narrow-band stochastic excited linear oscillator coupled to nonlinear energy sink

This paper draws attention to the issue of the vibration absorption of nonlinear mechanical system coupled to nonlinear energy sink(NES) under the impact of the narrow band stochastic excitation. Firstly, based on the complex-averaging method and frequency detuning methodology,response regimes of oscillators have been researched under the linear impact of coupling a nonlinear attachment with less relativistic mass and an external sinusoidal forcing, of which results turn out that the quasi-periodicity response regime of system which occurs when the external excitation amplitude exceeds the critical values will be the precondition of the targeted energy transfer.Secondly, basing on the path integration method, vibration suppression of NES has been researched when it is affected by a main oscillator with a narrow band stochastic force in the form of trigonometric functions, of which results show that response regimes are affected by the amplitude of stochastic excitation and the disturbance strength. Finally, all these conclusions have been approved by the numerical verification and coincided with the theoretical analysis; meanwhile, after the comparing analysis with the optimal linear absorber, it turns out that the NES which is affected by the narrow band stochastic force could also suppress the vibration of system with a better effect.     

Threshold Investigation of Phase-Locked Discriminators

This paper is primarily an investigaton of a second-order phased-locked loop in the threshold region, with the loop filter chosen as (1/1+?s) or (1+?1s/1+?s). First-order loop results are also given. Effects of loop parameters, detuning error, and modulation are studied. It is shown that the loop with filter (1+?1s/1+?s) can be built two ways with same bandwidth and damping. One loop gives much better threshold than the other. The analytical results are supported by computer simulation as well as experimental work obtained by hardware simulation of the loop.     

陀螺仪气室中碱金属原子数密度的检测

碱金属原子作为原子陀螺仪原子源的组成部分，其数密度是计算原子陀螺仪工作指标的重要参数。基于碱金属原子对不同激光失谐的吸收程度不同，提出了一种通过拟合碱金属原子吸收光谱得到碱金属原子数密度的测量方案。不同于以往的吸收测量法，该方案针对实际实验温度和气体压强等条件，对吸收谱拟合式进行了修正，从而提高了测量结果的准确度。测量结果与理论计算结果相吻合，两者偏差仅1.2倍左右，并可进一步应用于校准气室内碱金属蒸气的实际温度值。     

To a Matter of Increasing the Spectral Efficiency of Phase Radio-Technical Data Transmission Systems Operating under Strong Intersymbol Interference

This paper analyzes the possibility of increasing the spectral efficiency of phase radio-technical data transmission systems that operate under conditions of mutual interference of symbols when “transparency windows” are used. The conditions for emergency of “transparency windows” are defined, recommendations for their application with the purpose of increasing the spectral efficiency of communication systems being considered are presented. Changes in time characteristics of “transparency windows” are analyzed (their lengths over the range of channel symbol time duration) depending on the frequency detuning.     

齿轮的摇型节径振动及其减振法

在研究排除某型机减速器振动过大故障中发现齿轮的一种新型振动模态即摇型节径振动模态。本文研究了其振动特性并由此阐明了减速器振动过大的机理。提出了两种特殊的调频方法,可将在工作转速上、下边界内的两摇型节径模态共振移出边界以外。论证了阻尼衬筒和阻尼圈减振的有效性。经采用齿轮减振措施后,减速器振动降到很低水平。      

改进状态变量法及其计算机实现

改进状态变量法运用了等效电路的概念,建立了改进的状态向量方程,该方程中包含了确定状态向量初始值的约束条件并同时自动建立了初始值计算公式。这简化了初始值的计算工作,因此克服了传统的状态变量法在这方面的缺陷。该计算公式适用于任意激励、特别是冲激激励作用下的动态电路初始值的计算,简单实用。在此基础上,给出了改进状态变量法的计算机实现方法,其计算程序是一套系统完整的状态变量法分析程序,具有很强的电路适用性。     

旋翼桨尖涡模型及其在自由尾迹分析中的影响

 建立了一个旋翼桨尖涡初始涡核半径计算模型,用于消除旋翼自由尾迹分析中桨尖涡涡核半径依靠经验设定的现状。该方法利用涡量和涡矩守恒关系,考虑旋转效应的影响,并修正Vatistas涡量分布函数,得到了一个关于桨尖涡初始涡核半径与桨叶附着环量分布之间的非线性关系。将新建立的初始涡核模型同先前建立的涡核扩散与拉伸模型以微分方程初值问题的形式组成一个完整的桨尖涡模型,并将其应用于自由尾迹分析方法中,分别对两副模型旋翼的悬停尾迹进行分析。计算得到的桨尖涡初始涡核半径和展向位置与实验测量值的对比表明本文模型具有较高的准确性。此外,讨论了涡核湍流动量扩散效应在自由尾迹分析中的影响,分析表明该效应对自由尾迹分析的收敛性有重要影响。     

可修复结构破坏危险性分析

在全面考虑影响结构破坏危险性多种主要随机因素的基础上,重点研究了将定期检查时查出的破损结构修复并重新投入使用情况下的结构破坏危险性分析方法。建立了相应的分析模型,并以某型国产歼击机机翼主梁为例,给出了分析计算结果。结果表明：对于长寿命飞机结构,在使用后期,忽略修复并重新投入使用的结构将是偏危险的。     

多根管型装药固体火箭发动机初始压强峰影响因素研究

为了解多根管型装药固体火箭发动机实验时出现的过高的初始压强峰的问题，采用实验研究和理论分析相结合的方法，对点火药量、药柱数量、限燃面积对初始压强峰的影响进行了研究。结果表明：对于多根管型装药固体火箭发动机，发现点火药量对初始压强峰影响较小，减少点火药量不能有效降低初始压强峰；药柱数量和限燃面积对燃通比和初始压强峰影响较大，装药数量从7根减少为6根时，初始压强峰减小了57%；限燃面积为装药外表面面积的0.22倍时，初始压强峰消失。同时，得到了该类型装药的侵蚀函数，其临界燃通比为50.10。     

初始缺陷尺寸分布的尺寸效应研究

疲劳结构可能的开裂区域面积不同引起结构可能萌生裂纹的初始缺陷尺寸分布各异是造成"疲劳尺寸效应" 的一个可能解释。研究了试样测试部分尺寸大小与萌生裂纹的初始缺陷尺寸分布的关系,并建立了分析模型。模型利用已知的小尺寸试样的初始缺陷尺寸分布和大小试样的开裂面积比,推导出了相同条件下未知大尺寸试样的初始缺陷尺寸分布。这为结构完整性研究以及基于小裂纹扩展理论大尺寸试样的耐久性分析和疲劳全寿命预测打下基础,并为进一步研究"疲劳尺寸效应"创造了条件。     

基于线接触的回转二次曲面加工仿真研究

根据线接触加工回转二次曲面基本原理,建立基于磨粒磨损理论的线接触加工过程仿真模型,给出仿真流程并分析仿真过程各项参数的选取方法,最后基于此模型来研究加工参数如磨粒大小、工件初始面形和刀具初始面形对加工结果的影响,仿真结果表明工件和刀具初始面形对加工结果没有影响。     

喷雾运动初始条件问题的研究

根据所完成的流动环境中颗粒在初始区域内速度分布的测量结果，对颗粒运动初始条件的问题进行了全面的研究，提出了统计性，随机性和确定性的三种初始条件及其数学处理方法，在此基础上，应用喷雾两相流的数值方法，计算了喷雾的运动，比较了不同初始条件对计算结果的影响，并将所得计算结果与实验结果做了比较，两者符合较好。     

初始几何缺陷对加筋结构后屈曲分析的影响

采用考虑几何和材料双重非线性的弧长法分析了受初始几何缺陷影响的加筋壁板在轴压载荷作用下的后屈曲破坏过程.在分析中探讨了初始几何缺陷的大小及形态对加筋壁板极限承载能力和破坏模式的影响.计算结果表明,当初始缺陷的最大位移值超过蒙皮厚度的0.1倍时,将影响结构的承载性能.小于蒙皮厚度的0.1倍时,初始缺陷的形态和大小对结构的承载能力不产生明显影响,但影响结构的最终破坏模式.在后屈曲分析中可以以线性屈曲特征值法计算得到的一阶屈曲模态为初始缺陷的模式,初始缺陷最大位移值取蒙皮0.005~0.1倍之间.