非线性油膜支承裂纹转子振动特性分析

 以具有无限长轴承和无限短轴承支承的横向裂纹转子为研究对象,分析在非线性油膜力与横向裂纹联合作用时,Jeffcott转子的动力特性,并将其与刚性支承情况进行比较。结果表明轴承油膜力的存在对裂纹转子的振动影响较大,一般将降低转子的振动,这样势必增加转子裂纹故障诊断的难度。所以,在进行裂纹转子的故障诊断时,必须考虑到支承条件的影响,建立合理的动力学模型。     

公开密钥数字签名算法研究

数字签名是密码学中的重要课题之一,它是传统文件手写签名的模拟,能够实现用户对以电子形式存放的消息的验证。当算法公开时,在计算上不可能由加密密钥求解解密密钥,因而可以将加密密钥公开,即公开密钥。RSA密码是一种利用因数分解的困难性而设计的公钥密码。本文详述了RSA加密算法的实现以及如何利用RSA实现数字签名。     

MD5算法在双机热备份信息同步中的应用

在双机热备份算法中,主服务器与备份服务器之间保持信息及时同步至关重要,但传统的主备信息同步方式在效率和可靠性方面却存在着一定的缺陷。为更好地提高主备信息同步效率,本文提出采用MD5(M es-sage D igest 5)算法,对主服务器与备服务器的同步信息进行信息摘要运算,转化为定长字节的信息流后再进行同步。实践应用证明该方法可快速侦测出主、备服务器同步信息的差别,提高双机热备份信息同步的效率。     

鲁棒Kalman滤波及其在水下组合导航中的应用

在水下捷联惯导(SINS)/多普勒计程仪(DVL)组合导航系统中,当外部辅助信息受到野值等非高斯噪声污染时,选取调节因子γ为固定值将会降低基于Huber方法的鲁棒Kalman滤波(HRKF)算法的精度和鲁棒性。针对此问题,提出了一种基于马氏距离(MD)算法的调节因子自适应的鲁棒Kalman滤波(HRAKF)算法。首先利用MD算法对正常/异常的观测量进行辨识;进而建立γk递推关系式,并根据量测噪声特性对γ值进行实时调整;最后利用γk求取Huber权函数,并对量测噪声阵进行修正。选取8000s船载实测数据,分别利用Kalman滤波(KF)、HRKF及HRAKF算法进行水下组合导航半物理仿真试验。试验结果初步表明:在观测量受到野值或混合高斯分布噪声污染时,相较于KF和HRKF,HRAKF可实现更高精度、更加稳定的组合导航。     

基于北斗空时信息的安全通信方法

随着5G大规模商用和6G研发的启动,天地一体已成为未来移动通信发展的共识,然而空口边界被无限扩大,使无线通信安全面临着前所未有的严峻挑战,我国北斗三号卫星导航系统的全球位置信息服务为安全通信与定位导航的学科交叉提供了可能。提出了一种利用用户空时信息进行加密的安全通信方法,该方法是一种利用位置和时间唯一性的加密技术,通过北斗卫星导航系统的定位授时服务获取用户的空时信息,基于短报文业务实现信息共享,在传统加密算法的基础上提供额外安全层。该方法在密钥生成阶段提出了一种基于MD5信息摘要结合Logistic混沌映射的密钥生成算法(MD5-Logistic),使加密过程随位置变化而动态更新。仿真结果表明,该算法生成的密钥具有较高随机性,且有效降低了生成密文与明文间的相关性。在此基础上,为提升对定位误差的容忍能力,引入容忍距离概念,将解密范围从一点扩大为一个区域,使系统的鲁棒性及实用性得到显著提升。最后通过实测得到通信成功率与容忍距离间的关系,并给出合适的容忍距离。     

基于北斗空时信息的安全通信方法

随着5G大规模商用和6G研发的启动,天地一体已成为未来移动通信发展的共识,然而空口边界被无限扩大,使无线通信安全面临着前所未有的严峻挑战,我国北斗三号卫星导航系统的全球位置信息服务为安全通信与定位导航的学科交叉提供了可能。提出了一种利用用户空时信息进行加密的安全通信方法,该方法是一种利用位置和时间唯一性的加密技术,通过北斗卫星导航系统的定位授时服务获取用户的空时信息,基于短报文业务实现信息共享,在传统加密算法的基础上提供额外安全层。该方法在密钥生成阶段提出了一种基于MD5信息摘要结合Logistic混沌映射的密钥生成算法（MD5-Logistic）,使加密过程随位置变化而动态更新。仿真结果表明,该算法生成的密钥具有较高随机性,且有效降低了生成密文与明文间的相关性。在此基础上,为提升对定位误差的容忍能力,引入容忍距离概念,将解密范围从一点扩大为一个区域,使系统的鲁棒性及实用性得到显著提升。最后通过实测得到通信成功率与容忍距离间的关系,并给出合适的容忍距离。     

转子动力学研究中的若干问题

本文分析了当前转子动力学研究的状况及趋势,提出了对一些课题的展望。所讨论的问题为:滚动轴承引起的几种特殊的转子振动现象;篦齿式封严装置(气封)的气弹力;失调叶片盘的振动机理,挤压油膜轴承的工作机理,转轴裂纹的振动监视,螺桨盘的颤振涡动。      

航空声纳浮标定位的数据融合方法研究

声纳浮标由于受到多种随机因素的干扰,定位精度相差很大,在对具有一定散布海域的潜艇目标进行探测时,往往会投放多枚定位浮标,出现数据冗余的现象。针对这一问题,本文提出了浮标定位算法中的一种数据融合算法;并分析了加权融合和非线性最小二乘数据融合的方法,最后通过仿真验证了这种算法的有效性和可行性。     

基于MD5技术的认证校验应用

将MD5算法的基本描述移植到Windows平台，并组件化，有利于解决基于MD5的认证校验应用中遇到的开发技术多样性反复用困难等问题。通过分析、研究和大量的测试，最终完成了方案制定、应用系统原型的实现．从而验证了该解决方案的技术可行性。     

Ballistic missile track initiation from satellite observations

An algorithm is presented to initiate tracks of a ballistic missile in the initial exoatmospheric phase, using line of sight (LOS) measurements from one or more moving platforms (typically satellites). The major feature of this problem is the poor target motion observability which results in a very ill-conditioned estimation problem. The Gauss-Newton iterative least squares minimization algorithm for estimating the state of a nonlinear deterministic system with nonlinear noisy measurements has been previously applied to the problem of angles-only orbit determination using more than three observations. A major shortcoming of this approach is that convergence of the algorithm depends strongly on the initial guess. By using the more sophisticated Levenberg-Marquardt method in place of the simpler Gauss-Newton algorithm and by developing robust new methods for obtaining the initial guess in both single and multiple satellite scenarios, the above mentioned difficulties have been overcome. In addition, an expression for the Cramer-Rao lower bound (CRLB) on the error covariance matrix of the estimate is derived. We also incorporate additional partial information as an extra pseudomeasurement and determine a modified maximum likelihood (ML) estimate of the target state and the associated bound on the covariance matrix. In most practical situations, probabilistic models of the target altitude and/or speed at the initial point constitute the most useful additional information. Monte Carlo simulation studies on some typical scenarios were performed, and the results indicate that the estimation errors are commensurate with the theoretical lower bounds, thus illustrating that the proposed estimators are efficient     

双轴应力下含裂纹加筋曲板剩余强度的弹塑性有限元计算

 采用考虑了大应变的弹塑性有限元方法,以裂纹尖端张开角为断裂准则,实现了双向受载条件下加筋曲板中裂纹起裂到失稳整个扩展过程的数值模拟计算;还对与加筋曲板有同样尺寸的加筋平板进行了分析和计算。结果表明,所提出的分析方法和所采用的断裂准则适用于对含裂纹加筋结构所进行的剩余强度分析。     

含多裂纹连接结构损伤容限试验研究

 针对机翼典型对接结构,进行了平板空孔试样和螺栓搭接件在等幅谱及飞－续－飞谱下的多裂纹损伤容限试验,通过该试验开展多裂纹开裂模式及多裂纹扩展规律的试验研究,为多裂纹断裂力学理论分析、多裂纹结构剩余强度准则提供试验依据。     

EM-ML algorithm for track initialization using possibly noninformative data

Initializing and maintaining a track for a low observable (LO) (low SNR, low target detection probability and high false alarm rate) target can be very challenging because of the low information content of measurements. In addition, in some scenarios, target-originated measurements might not be present in many consecutive scans because of mispointing, target maneuvers, or erroneous preprocessing. That is, one might have a set of noninformative scans that could result in poor track initialization and maintenance. In this paper an algorithm based on the expectation-maximization (EM) algorithm combined with maximum likelihood (ML) estimation is presented for tracking slowly maneuvering targets in heavy clutter and possibly noninformative scans. The adaptive sliding-window EM-ML approach, which operates in batch mode, tries to reject or weight down noninformative scans using the Q-function in the M-step of the EM algorithm. It is shown that target features in the form of, for example, amplitude information (AI), can also be used to improve the estimates. In addition, performance bounds based on the supplemented EM (SEM) technique are also presented. The effectiveness of new algorithm is first demonstrated on a 78-frame long wave infrared (LWIR) data sequence consisting of an Fl Mirage fighter jet in heavy clutter. Previously, this scenario has been used as a benchmark for evaluating the performance of other track initialization algorithms. The new EM-ML estimator confirms the track by frame 20 while the ML-PDA (maximum likelihood estimator combined with probabilistic data association) algorithm, the IMM-MHT (interacting multiple model estimator combined with multiple hypothesis tracking) and the EVIM-PDA estimator previously required 28, 38, and 39 frames, respectively. The benefits of the new algorithm in terms of accuracy, early detection, and computational load are illustrated using simulated scenarios as well.     

Track-While-Scan Algorithm in a Clutter Environment

A track-while scan (TWS) algorithm is developed for targets in a clutter environment. The problem has been studied using only the position measurements [1, 5-8], but the simulation results have not been satisfactory. Modern processing techniques (FFT processor) ) in air traffic control and surveillance radar receivers provide both position and radial velocity. The radial velocity measurement may be conveniently used in the target-track correlation process, which will reduce the association ambiguity in the clutter environment. t. In the clear environment the algorithm using the position and radial velocity measurements has been treated in [3, 4]. A TWS algorithm, using both position and radial velocity measurements for targets in a clutter environment, is presented here. The algorithm obtained is nonlinear and adaptive. In order to evaluate the improvement due to radial velocity measurement a simulation has been performed on a digital computer. The algorithm was run with and without radial velocity measurements to compare its performances. An improvement was noted especially when the target path included an accelerated portion.     

航空发动机涡轮盘榫齿裂纹故障研究

B型机由A型机改型而成,大批服役期中的A型机存在着大量Ⅱ级盘(简称为盘)第一榫齿裂纹与掉块故障。其轻者,裂纹超过标准后报废;重者,榫齿掉块,打伤其它零件,甚至叶片飞出(简称脱榫)。经过故障件金相检查,断口分析,其裂纹性质属机械疲劳。在疲劳损伤中,叶片类零件主要是高循环疲劳。为排除B型机盘和叶片榫齿间连接的故障,我们研究了在飞行与试车台上A、B型机Ⅱ级涡轮叶片(简称为叶片)的振动情况。      

纤维金属层板疲劳裂纹扩展速率与寿命预测的唯象模型

以纤维金属层板疲劳裂纹稳定扩展的特性为基础,提出了纤维金属层板等效裂纹长度（l0）的概念,导出了纤维金属层板疲劳过程中的有效应力强度因子方程,建立了纤维金属层板等幅疲劳下疲劳裂纹扩展速率与寿命预测的唯象模型。它不仅适用于中心裂纹,同时也适用于边缘裂纹。用唯象模型对2/1GLARE和3/2GLARE层板的CCT试样和SENT试样进行了寿命预测,并与试验结果进行了对比。当裂纹从锯切裂纹尖端扩展到试样宽度的80%时,对于GLARE层板的CCT试样,2/1GLARE层板的预测寿命与实测寿命之比为1.05,3/2GLARE层板的预测寿命与实测寿命之比为1.07.对于GLARE层板的SENT试样,预测寿命与实测寿命之比为1.12.唯象模型不仅预测结果可靠,精度高,而且都是解析运算,非常方便。唯象模型的提出使得纤维金属层板的疲劳裂纹扩展速率和寿命的预测变得跟金属材料一样方便,因此具有重要的工程应用价值。     

遗传算法在飞行冲突解脱中的应用分析

国内外的专家和学者研究过多种方法用于飞行冲突解脱及解脱成本最小化问题,本文主要简介了基于遗传算法对2架飞机的飞行冲突的解脱模型,并在实际应用中对原来的优化过程进行了修改和完善,以某大型客机巡航参数为例,计算了优化后的飞行成本,结果表明:重新改进后的优化轨迹能够进一步降低飞行成本。     

基于运动捕捉系统的多旋翼飞行器实时测姿算法

旋翼飞行器的室内自主飞行是目前研究的热点之一。在室内飞行过程中,飞行器姿态和位置信息可以通过运动捕捉系统（Motion Capture System,MCS）来进行实时测量,从而为机载低成本MEMS惯性导航系统提供校正信息。结合四旋翼飞行器的结构特性,提出了一种五点实时测姿算法。相对于目前MCS常用的测姿算法,该算法可以降低标记点安装引起的测姿误差。室内实验结果表明,该算法测姿精度高,并且能够有效实现四旋翼飞行器室内动态实时姿态测量,具有较好的工程应用价值。     

裂纹叶片振动特性研究

建立应用传递矩阵法求解裂纹叶片振动特性的方法,以矩形截面裂纹悬臂梁为计算实例,分析了沿叶宽等深度扩展的横向裂纹位置、深度对其弯曲型振动特性的影响。选用方波函数模拟裂纹开合过程,理论分析了裂纹叶片的非线性振动特性。通过裂纹试件实验,对理论研究方法和结果做了验证。提出了叶片裂纹故障在线监测特征量的选择建议     

Consensus based on learning game theory with a UAV rendezvous application

Multi-agent cooperation problems are becoming more and more attractive in both civilian and military applications. In multi-agent cooperation problems, different network topologies will decide different manners of cooperation between agents. A centralized system will directly control the operation of each agent with information flow from a single centre, while in a distributed system, agents operate separately under certain communication protocols. In this paper, a systematic distributed optimization approach will be established based on a learning game algorithm.The convergence of the algorithm will be proven under the game theory framework. Two typical consensus problems will be analyzed with the proposed algorithm. The contributions of this work are threefold. First, the designed algorithm inherits the properties in learning game theory for problem simplification and proof of convergence. Second, the behaviour of learning endows the algorithm with robustness and autonomy. Third, with the proposed algorithm, the consensus problems will be analyzed from a novel perspective.