Experimental and Numerical Investigation of the Effects of Passive Vortex Generators on Aludra UAV Performance

A study of the effects of passive vortex generators (VGs) on Aludra unmanned aerial vehicle (UAV) aerodynamic characteristics is presented. Both experimental and numerical works are carried out where an array of VGs is attached on Aludra UAV’s wing. The flow measurements are made at various angles of attack by using 3-axis component balance system. In the numerical investigation, the Reynolds-averaged Navier-Stokes (RANS) code FLUENT 6.3TM is used in the simulations with fully structured mesh with Spalart-Allmaras (S-A) turbulence model and standard wall function. The comparison between the experimental and numerical results reveals a satisfactory agreement. The parametric study shows that higher maximum lift coefficient is achieved when the VGs are placed nearer to the separation point. In addition to this, shorter spanwise distance between the VGs also increases the maximum lift coefficient, rectangular and curve-edge VG performs better than triangular VG.     

Maneuvering Target Tracking in Dense Clutter Based on Particle Filtering

An improved particle filtering(IPF) is presented to perform maneuvering target tracking in dense clutter.The proposed filter uses several efficient variance reduction methods to combat particle degeneracy,low mode prior probabilities and measure-ment-origin uncertainty.Within the framework of a hybrid state estimation,each particle samples a discrete mode from its poste-rior distribution and the continuous state variables are approximated by a multivariate Gaussian mixture that is updated by an unscented Ka...     

Update Chain-based Approach for Checking Route Oscillation of BGP

This paper presents a novel approach for checking route oscillation of border gateway protocol(BGP) quickly,by which the privacy of routing policies of autonomous system(AS) can be respected.Firstly,route update chain tag(RUCT) is constructed to track the forwarding of update report,and local routing library is made to record the changing history of update report.Then route oscillation can be identified by analyzing correlative state of RUCT and local routing library.The characteristic of this approach is that an arbitrary AS can check route oscillation alone only by sharing its network ID,which greatly respects the pri-vacy of routing policies for each AS.This paper shows that both looping in RUCT and consecutive positive-negative report in local record are sufficient conditions for route oscillation.Comparative experiments demonstrate the availability and efficiency of the proposed approach.     

Research of Compound Controller for Flight Simulator with Disturbance Observer

A compound controller is proposed to alleviate the considerable chattering in output of zero phase error tracking controller (ZPETC), when the flight simulator losses command data of simulation signal. Besides, the shortcomings, caused by conventional differential methods in retrieving velocity and acceleration signals, are avoided to a certain extent. The compound controller based on disturbance observer (DOB) is composed of a feed-forward controller and a feedback controller. It estimates velocity and acceleration of unknown tracking signal, and also velocity response with an approximate method for differential. The experiments on a single-axis flight simulator show that the proposed method has strong robustness against parameter perturbations and external disturbances, owing to the introduced DOB. Compared with the scheme with ZPETC, the proposed scheme possesses more simple design and better tracking performance. Moreover, it is less sensitive to position command distortion of flight simulator.     

Research of Optical Fiber Coil Winding Model Based on Large-deformation Theory of Elasticity and Its Application

Optical fiber coil winding model is used to guide proper and high precision coil winding for fiber optic gyroscope (FOG) application. Based on the large-deformation theory of elasticity, stress analysis of optical fiber free end has been made and balance equation of infinitesimal fiber is deduced, then deformation equation is derived by substituting terminal conditions. On condition that only axial tensile force exists, approximate curve equation has been built in small angle deformation scope. The comparison of tangent point longitudinal coordinate result between theory and approximation gives constant of integration, and expression with tangent point as origin of coordinate is readjusted. Analyzing the winding parameters of an example, it is clear that the horizontal distance from the highest point of wheel to fiber tangent point has millimeter order of magnitude and significant difference with fiber tension variation, and maintains invariant when wheel radius changes. The height of tension and accurate position of tangent point are defined for proper fiber guide. For application to fiber optic gyroscope, spiral-disc winding method and nonideal deformation of straddle section are analyzed, and then spiral-disc quadrupole pattern winding method has been introduced and realized by winding system. The winding results approve that the winding model is applicable.     

基于速度观测器的模型参考自适应摩擦补偿

具有相对运动的机械伺服系统中都存在着摩擦干扰力矩。针对机械伺服系统不能提供速度信号时的摩擦补偿问题 ,本文提出了一种基于速度观测器的模型参考自适应摩擦补偿方法 ,该方法利用一降维观测器在线估计速度信号 ,并根据该估计信号构成模型参考自适应摩擦补偿器。根据摩擦补偿器构成的两种情况 ,对系统误差的收敛性进行了分析 ,并进行了仿真验证 ,仿真结果说明了该方法的有效性和可行性     

债转股问题初探

债转股作为经济体制改革的一个重要探索，已经成为当今法学界和经济学界讨论的主题。作为一个新事物的出现，债转股必然会遇到一系列来自不同方向的阻碍，本文就这些困惑进行论述，阐明了债转股面临的主要问题，并提出相应的解决方案和建议。国民经济体制改革需要大胆的探索和创新，债转股就是一个很好的范例，尽管其实施过程中难免遇到一些难题，但必将取得骄人的成果。     

浅谈作业成本计算

作业成本计算(Activity—Based Costing，简称ABC)是西方国家于八十年代末开始研究、九十年代以来在先进制造企业首先应用起来的一种全新的企业管理理论和方法。本文从作业成本计算冲破了传统成本计算的思维模式，为企业的经营管理提供了更加准确监控信息的角度，对作业成本计算的基本原理进行了粗浅的探讨。随着计算机在管理中的广泛应用，作业成本计算必将成为一种新的现代管理方法受到企业管理者的青睐。     

企业集团开展内部审计工作初探

企业集团是以资本(产权关系)为主要纽带，通过持股、控股等方式紧密联结、协调行动的企业群体。它与其他企业相比，具有许多独特之处。本文仅从内部审计的角度，就企业集团内部审计的特点、机构设置的原则和职能，以及内部审计风险的防范等方面进行初步探讨，以期使我国企业集团的内部审计工作早日步入规范化轨道，真正发挥其对经济工作的监督和促进作用。     

固体发动机壳体工作状态塑性流动数值模拟

采用二维轴对称模型及有限元数值计算方法，对固体火箭发动机壳体在高压下的应力分布进行了分析和计算，获得了发动机壳体在工作条件下的塑性形变及应力场的分布。其结果可供基于塑性形变的壳体评估及可靠性设计参考。