基于视景通道的透镜成像过程仿真技术研究

针对计算机成像模型在使用过程中存在的不足,提出了对该模型进行完善与改进的方法。首先根据数字变焦原理,推导出放大倍率与视锥角的关系公式,实现了视景通道的变焦功能,该方法计算量小,效果逼真;其次,提出了一种镜头对焦过程的仿真方法,它充分利用粒子系统技术模拟对焦成像由模糊到清晰的过程,不仅获得更真实的图像效果,且满足实时性要求。上述改进后模型与实际摄像系统原理基本一致,增强了仿真系统视觉效果逼真性与沉浸感。由于该方法在工程上极易实现,可以在虚拟现实系统中广泛应用。

Abstract：

A way that could be improved was brought forward on the pin-hole camera model in allusion to the problems of the insufficient cue of depth. The relation formulas of the magnification and aspect angle were concluded according to the principles of digital zoom and the zooming function of visual channels was realized. The implementation of this method is simple and the effect is realistic. Besides,a simulation method for the course of adjusting focus was proposed,which brought blurry images into focus by particle system. Both vivid images and real time requirement could be achieved. The ameliorated model runs in the same way as the real camera system on the theory,thus enhancing the fidelity and immersion of visual effects. It is so easy to implement in project that this approach can be used universally in VR systems.     

Multi-dimensional scattering properties diagnosis system of scale aircraft model in an anechoic chamber

Aiming at the concept of ＂diagnosis＂, a simple and effective broadband radar cross section （RCS） measurement system is constructed, and some multi-dimensional scattering properties diagnosis techniques are presented based on the system. Firstly, a stepped-frequency signal is employed to achieve high range resolution, combining with a variety of signal processing tech- niques. Secondly, cross-range resolution is gained with a rotating table, and the high-resolution two-dimensional （2-D） imaging of the scale model is obtained by the microwave imaging theory. Finally, two receiving antennas with a small distance in altitude are used, and the three-dimensional （3-D） height distribution of scattering points on the scale model is extracted from the phase of images. Some typical bodies and a scale aircraft model are diagnosed in an anechoic chamber. The experimental results show that, after scaling with a metal sphere, the accurate one- dimensional （l-D） RCS pattern of the model is obtained, and it has a large dynamic range. When the bandwidth of the transmitting signal is 4 GHz, the resolution of the 2-D image can reach to 0.037 5 m. The 3-D height distribution of scattering points is given by interferometric measurement. This paper provides a feasible way to obtain high-precision scattering properties parameters of the scale aircraft model in a conventional rectangular anechoic chamber.     

单线列车运行调整的梯度搜索算法仿真与研究

列车运行调整的优化是一个非常复杂的问题,需考虑的因素很多,很难给出一个完美的优化模型。根据单线列车运行调整的特点,建立了单线列车运行图的离散事件拓扑图模型,提出了＂调整运行图综合满意度＂作为运行调整的目标,并进一步论证了＂调整运行图综合满意度＂函数的单调递减特性;提出了冲突树的概念和梯度搜索算法的算法原理及搜索步骤,并实例进行仿真。仿真结果表明,该算法模型在实际运行过程中的具有较好的优化性和有效性。

Abstract：

The optimization of railway rescheduling is a very complex issue, many factors should to be taken into account, and it’s difficult to give a perfect optimization model. A discrete event topologic diagram model was derived according to the characteristics of the single-track railway diagram, and the ＂comprehensive satisfaction of the adjusted train diagram＂ was proposed as the target of the railway rescheduling, then the monotonically decreasing characteristic of the target function was demonstrated. The concept of conflict tree was developed and the principle and steps of the gradient search algorithm based on the DET model were given and simulated. The simulation results show that this algorithm has better adaptability and effectiveness in practical application.     

Optimal aeroassisted symmetric transfer between coplanar elliptical orbits

The problem of optimal aeroassisted symmetric transfer between elliptical orbits is concerned.The complete trajectory is assumed as consisting of two impulsive velocity changes at the beginning and the end of an interior atmospheric subarc,where the vehicle is controlled via the lift coefficient and thrust.The corresponding dynamic equations are built and bounded controls are considered.For the purpose of optimization computation,the equations are normalized.In order to minimize the total fuel consumption,the geocentric radius of initial elliptical transfer orbital perigee and controls during atmospheric flight should all be optimized.It is an optimal control problem which involves additional parameter optimization.To solve the problem,a two-level optimization method denoted by "genetic algorithm + Gauss pseudospectral method" is adopted:the genetic algorithm is used for parameter optimization and the Gauss pseudospectral method is used for optimal control problems.The flow chart of simulation is given.On this basis,the issue of more realistic modeling with two finite-thrust subarcs in the nonatmospheric part of the trajectory is simultaneously addressed.The orbital transfer problem is transformed to three continuous optimal control problems,and the constraints at different times are given,which are respectively solved by using the Gauss pseudospectral method.The obtained numerical results indicate that the optimal thrust control is of bangbang type.The minimum-fuel trajectory in the atmosphere consists of aeroglide,aerocruise and aeroglide.They are compared with the results of pure impulsive model,and the conclusions that a significant fuel saving will be achieved by synergetic maneuver are drawn.     

编队箔条弹与舰空导弹武器火力兼容模型

编队箔条弹干扰与舰空导弹协同防空作战中的火力兼容控制属于编队软硬武器火力兼容控制的一种基本情况。通过建立编队坐标系中箔条云假目标位置变化动态模型和舰空导弹起控点参数模型,从箔条云对雷达电磁波散射的角度出发,提出了基于箔条云对电磁波衰减特性的箔条弹与舰空导弹火力兼容判别模型,通过协同控制编队中舰空导弹的发射时间,避免了箔条弹对导弹的干扰,解决了二者之间的火力冲突。研究成果有助于提高编队防空作战能力,并为编队其它软硬武器火力兼容研究提供借鉴。

Abstract：

The firepower compatibility of fleet chaff jamming and ship-to-air missile cooperative air defense is one of the basic forms of fleet hard and soft weapon firepower compatibility.The model of chaff cloud decoy target moving and the guidance starting point position model of ship-to-air missile were established.Based on the characteristic of electromagnetic scattering from chaff cloud and the attenuation of chaff cloud to electromagnetic waves,the firepower compatibility model of fleet chaff jamming and ship-to-air missile was given.By controlling the time of missile launched,the jamming from chaff clouds could be avoided,and the conflicts between chaff jamming shell and missile were solved.The model can be used for reference researches in this area.     

On implementing the symbolic preprocessing function over Boolean polynomial rings in Gröbner basis algorithms using linear algebra

Some techniques using linear algebra was introduced by Faugère in F4 to speed up the reduction process during Gr?bner basis computations.These techniques can also be used in fast implementations of F5 and some other signature-based Gr?bner basis algorithms.When these techniques are applied,a very important step is constructing matrices from critical pairs and existing polynomials by the Symbolic Preprocessing function(given in F4).Since multiplications of monomials and polynomials are involved in the Symbolic Preprocessing function,this step can be very costly when the number of involved polynomials/monomials is huge.In this paper,multiplications of monomials and polynomials for a Boolean polynomial ring are investigated and a specific method of implementing the Symbolic Preprocessing function over Boolean polynomial rings is reported.Many examples have been tested by using this method,and the experimental data shows that the new method is very efficient.     

Improved fuzzy identification method based on Hough transformation and fuzzy clustering

This paper presents an approach that is useful for the identification of a fuzzy model in SISO system. The initial values of cluster centers are identified by the Hough transformation, which considers the linearity and continuity of given input-output data, respectively. For the premise parts parameters identification, we use fuzzy-C-means clustering method. The consequent parameters are identified based on recursive least square. This method not only makes approximation more accurate, but also let computation be simpler and the procedure is realized more easily. Finally, it is shown that this method is useful for the identification of a fuzzy model by simulation.     

Stability of GM(1,1) power model on vector transformation

The morbidity problem of the GM(1,1) power model in parameter identification is discussed by using multiple and rotation transformation of vectors. Firstly we consider the morbidity problem of the special matrix and prove that the condition number of the coefficient matrix is determined by the ratio of lengths and the included angle of the column vector, which could be adjusted by multiple and rotation transformation to turn the matrix to a well-conditioned one. Then partition the corresponding matrix of the GM(1,1) power model in accordance with the column vector and regulate the matrix to a well-conditioned one by multiple and rotation transformation of vectors, which completely solve the instability problem of the GM(1,1) power model. Numerical results show that vector transformation is a new method in studying the stability problem of the GM(1,1) power model.     

A MATHEMATICAL PROGRAMMING MODEL FOR THE COEXISTENCE OF COMPETITIONS AND COOPERATIONS PROBLEMS

We study in this paper a mathematical programming model for the coexistence of competitions and cooperations problems. We introduce a new solution concept, s-optimal solution for the problem, which always exists under compact and continuous conditions. It is shown that an s-optimal solution can be obtained by solving a nonlinear programming problem. Some examples are given to explain how to compute an s-optimal solution.     

An analytic hierarchy process model of group consensus

In group decision making, a certain degree of consensus is necessary to derive a meaningful and valid outcome. This paper proposes a consensus reaching model for a group by using the Analytic Hierarchy Process （AHP）. It supports people to improve their group consensus level through an updating of their judgments. In this model, a moderator suggests the most discoraant aeclslon manet to update his judgment in each step. The proposed consensus reaching model allows decision makers to accept or reject the suggestion from the moderator. This model ensures that the judgment updating is effective and the final solution will be of acceptable consistency. Finally, a numerical example is given to illustrate the validity of the proposed consensus reaching model.     

降低时间延迟的紫外光通信系统设计

针对紫外光大气传输理论和非直视单散射模型,分析了大气信道对紫外光通信的影响,并在不同参数条件下,对大气信道所产生的时间延迟进行了定量仿真。仿真结果表明：时,可延迟／疃通信距离的增加而迅速增大,通信距离增加1km,时间延迟增加约2倍;时间延迟随发射和接收仰角的增加而增加,且发射仰角对时间延迟的影响大于接收仰角;时问延迟压壅发射束散角和接收视场角的增咖而减小。因此,为减小通信系统的时间延迟,在紫外光通信系统设计时,应尽量减小系统的发射仰角和接收仰角,增加系统的发射束散角和接收视场角。     

海面舰船场景的视频图像海雾去除算法

为满足海面舰船视频图像海雾去除的实时性要求,提出一种基于引导滤波的快速视频图像海雾去除方法。针对单幅图像,根据经典大气散射物理模型,首先利用暗原色先验估计大气光值和初始透射率,然后利用引导滤波优化透射率,进而求解大气散射物理模型,实现快速去雾;针对视频图像,结合帧差法和引导滤波,利用引导滤波估计视频帧序列的雾气遮罩,实现快速去雾。与其他单幅图像和逐帧视频图像去雾算法分别进行实验仿真对比研究,从主观和客观两方面进行处理结果的图像质量评价。结果表明,所提算法能实现快速海雾去除、有效提高视频去雾效率。     

用于飞行实时仿真的微下击暴流建模研究

分析了微下击暴流的特征和用于飞行实时仿真中的建模需求。基于流体力学的涡环原理构建三维微下击暴流的参数化模型,并对涡环法建模进行了深入改进。基于流体力学方法解决了涡环法模型的中心轴处和涡核内的奇异问题。针对真实微下击暴流风场的特点,设计了倾斜涡环模型和多涡环模型,从而高逼真度地模拟复杂的微下击暴流风场。简要讨论了该模型在飞行实时仿真中的应用方法。该建模方法灵活性高,可重配置,不仅可用于变化风场中的飞行实时仿真,还可用于对实际风场测量数据进行辨识建模和再现研究。     

机载气象雷达的三维湍流模型和探测仿真方法

对湍流等复杂气象目标的探测仿真是研究复杂气象目标的有效方法,为了提高机载气象雷达对湍流目标的探测仿真系统的精度,提出一种新的基于蒙特卡罗原理的大气湍流三维建模方法。基于相关函数矩阵生成了Von Karman湍流模型,将该模型应用到机载气象雷达湍流目标检测系统中,通过该数学模型生成湍流的雷达回波模型,对湍流目标的多普勒速度和谱宽进行估计和分析。仿真结果表明,该模型可以满足机载气象雷达湍流目标仿真时对湍流风场数值的要求,通过理论分析与仿真数值的相关性检验对比,证明所提仿真模型符合理论模型特征且具有较高的仿真精度,满足大气湍流的统计特性。通过与Dryden模型在湍流探测仿真结果进行对比,所提模型更接近于真实风场特点。     

基于偏微分方程的户外图像去雾方法

户外图像的雾化往往导致色彩降质和对比度降低,有效的去除图像中天气效果对提高视觉系统的可靠性和鲁棒性具有重要意义。根据大气散射物理模型以及有雾图像的色彩与对比度降质同场景点的景深成指数关系的先验知识,分别建立了户外图像全局去雾和局部去雾的能量最优化模型,推导了相应的求解偏微分方程。利用用户提供的简单附加信息,实现了仅从单幅图像恢复清晰图像的去雾算法。实验结果表明：去雾图像的色彩清晰度和对比度有较大改善,具有很好的应用前景。     

Feature Extraction of Localized Scattering Centers Using the Modified TLS-Prony Algorithm and Its Applications

Feature Extraction of Localized Scattering Centers Using the Modified TLS-Prony Algorithm and Its Applications~~~~     

空面导弹系统的建模与仿真

简要介绍了模块化设计思想，然后将其应用于空面导弹系统的建模，分需求分析、功能分析与分解、模块划分及模块设计与开发四个步骤，建立了空面导弹仿真模型库，它主要包括导航系统、制导系统和弹体这三个子系统．最后，为了检验模型库的可用性，针对某型空面导弹进行了仿真研究。从仿真结果来看，各子系统的仿真模型具有较高的保真度，能够满足实时性、快速性的要求。     

一对一超视距空战仿真中的机载雷达模型研究

为提高一对一超视距空战仿真的置信度,在考虑多路径效应、杂波、电子干扰、脉冲积累以及PRF选择的基础上,运用功能仿真法建立超视距空战机载雷达的数学模型。采用数值模拟法给出一对一超视距空战的仿真流程,以领先跟踪概率、跟踪距离、跟踪时间作为探测效能指标,运用蒙特卡洛法分析雷达自身性能和电子对抗方案对探测效能的影响。结果表明,此模型能够较好地模拟超视距空战中机载雷达的探测过程,合理可行。     

高速运动目标ISAR回波的基带模拟

分析了高速运动目标对采用大时带积信号的ISAR雷达回波的影响,然后建立回波信号模型,产生仿真试验结果;最后,基于散射中心模型构造动目标,产生给定动态参数下的动目标ISAR回波信号数据,并结合带有D/A的FPGA开发板产生动目标的ISAR回波信号,为ISAR的研究和数据处理提供了信号源。     

飞行载体上低副瓣共形天线阵的综合

本文给出了在考虑飞行载体对天线阵性能影响的情况下,低副瓣共形天线阵的综合方法,并针对给定的载体形式,对某一共形阵进行了综合。结果表明,载体的影响可以通过适当的激励加以补偿,使天线在实际工作环境中具有良好的性能。