拱坝体型的多目标博弈设计

提出基于博弈理论的多目标求解方法,给出多目标问题的博弈描述和各博弈方策略空间的计算方法,研究:1)利用Nash均衡模型求解无目标偏好的多目标竞争问题;2)利用Stackelberg寡头模型求解有目标偏好的多目标竞争问题;3)利用合作竞争模型求解关注整体得益的多目标设计问题;并给出相应的技术步骤.以白鹤滩拱坝体型的三目标博弈设计为例,取体积目标、坝体最大主拉应力目标和坝体应变能目标为博弈方,分别采用Nash均衡模型、Stackelberg寡头模型和合作竞争模型进行博弈求解,设计结果显示拱坝的体积方量、应力、应变能和位移等较初始体型的变化改善情况,实现了各博弈模型的设计目的,表明了多目标博弈设计方法的有效性.     

GENERALIZED VARIATIONAL DATA ASSIMILATION METHOD AND NUMERICAL EXPERIMENT FOR NON-DIFFERENTIAL SYSTEM

The generalized variational data assimilation for non-differential dynamical systems is studied. There is no tangent linear model for non-differential systems and thus the general adjoint model can not be derived in the traditional way. The weak form of the original system was introduced, and then the generalized adjoint model was derived. The generalized variational data assimilation methods were developed for non-differential low dimensional system and non-differential high dimensional system with global and local observations. Furthermore, ideas in inverse problems are introduced to 4DVAR ( Fourdimensional variational ) of non-differential partial differential system with local observations.     

Aerodynamic optimization of 3D wing based on iSIGHT

A method for combining the CFD software,Fluent,with the iSIGHT design platform is presented to optimize a three-dimensional wing to ameliorate its aerodynamics performance.In the optimization design,two kinds of genetic algorithms,the Neighborhood Cultivation Genetic Algorithm（NCGA）and the Non-dominated Sorting Genetic Algorithm（NSGAII）,are employed and the Navier-Stoke（N-S）equations are adopted to derive the aerodynamics functions of the 3D wing.The aerodynamic performance of the optimized wing has been significantly improved,which shows that the approach can be extended and employed in other cases.     

激光陀螺捷联惯导减振系统动力学建模与仿真

由于激光陀螺固有机抖频率的存在,以及导弹运输、装卸、发射与飞行过程经历的动态环境中振动、冲击、过载等激励,导致激光陀螺在导弹上使用输出精度差。应用多体系统传递矩阵法,建立了激光陀螺捷联惯性测量组合减振多体系统动力学模型,分析激光陀螺固有抖动和导弹振动冲击对激光陀螺输出精度的影响。通过对减振系统动力学模型进行仿真,获得了激光陀螺抖动和导弹冲击环境下激光陀螺捷联惯性测量组合减振系统动态响应。该仿真结果为激光陀螺捷联惯性测量组合减振设计提供理论依据,该分析方法为激光陀螺捷联惯组在导弹上应用提供理论基础。     

完整系统的多刚体系统离散时间传递矩阵法研究

基于多刚体系统离散时间传递矩阵法,采用提高计算精度的方法,研究具有大运动、非线性特征的完整系统在平面、空间中的动力学响应.提出了对部分变量重新赋值的违约修正方法,计算机仿真表明了其有效性.多刚体系统离散时间传递矩阵法不须进行违约修正,体现了该方法建模灵活性较强、程式化程度较高的优点.     

Multi-objective optimization design of radar absorbing sandwich structure

By introducing a dimensionless parameter to couple the two objectives, weight and radar absorbing performance, into a single objective function, a multi-objective optimization procedure for the radar absorbing sandwich structure （RASS） with a cellular core is proposed. The optimization models considered are one-side clamped sandwich panels with four kinds of cores subject to uniformly distributed loads. The average specular reflectivity calculated with the transfer matrix method and the periodic moment method is utilized to characterize the radar absorbing performance, while the mechanical constraints include the facesheet yielding, core shearing, and facesheet wrinkling. The optimization analysis indicates that the sandwich structure with a two-dimensional （2D） composite lattice core filled with ultra-lightweight sponge may be a better candidate of lightweight RASS than those with cellular foam or hexagonal honeycomb cores. The 2D Kagome lattice is found to outperform the square lattice with respect to radar absorbing.     

约束最优控制理论及其在气动优化中的应用

为了隐式地和自动地处理气动优化中的约束条件,在Jameson的无约束控制论气动优化设计理论基础上发展了有约束的最优控制理论,建立了约束伴随方程方法,并将其成功地应用到了约束气动优化设计中.比较约束伴随方法和Jameson的原始方法,约束优化问题仅仅只需要修改最终伴随方程的物面边界条件和梯度的计算公式而其它项与Jameson原始方法中的完全相同.这表明了基于控制理论的优化方法不仅适用于含有大量设计变量的优化问题,而且也可以很方便地处理约束优化问题.     

含多处裂纹梁的振动分析

基于传递矩阵方法,提出了一种计算含有任意处裂纹梁固有频率的新方法.将梁内裂纹模拟为无质量的弯曲弹簧,得到了梁的解析特征方程.通过数值模拟计算,讨论了裂纹数量,以及裂纹位置和裂纹深度对梁的固有频率的影响.通过与文献[4]的计算结果比较,验证了本文方法的有效性.     

层体边界元法在二维层体断裂分析中的应用

在刚度矩阵法的基础上建立了用于进行二维多层体结构断裂分析的边界单元法（ＢＥＭＬＭ）由于ＢＥＭＬＭ的基本方程中已经包含了层体表面和裂纹缝面的边界条件，因而不需要对这些边界进行单元离散，从而其断裂分析可望有较好的精度通过与柯西积分方程法进行结合，算例表明ＢＥ ＭＬＭ是可靠并有效的     

Mathematica 在传递矩阵法中的应用

通过两个具体实例,说明了Ｍａｔｈｅｍａｔｉｃａ在传递矩阵法中的应用．特别介绍了用Ｒｅｄｕｃｅ命令求振动系统固有频率的方法,并把所得结果与已有结果作了对比,显示了这一方法的优越性．     

多体系统动力学动态最优化设计与灵敏度分析

基于多体系统的动态最优化设计过程包括传统的多体系统仿真分析、系统设计灵敏度分析、 系统最优化设计等过程, 针对多体系统运动学、用二阶常微分方程和微分代数方程描述 的动力学,基于含设计参数的通用数学模型及通用的积分型目标函数,采用高效的系统灵 敏度分析伴随变量方法及易于实施的惩罚函数最优设计方法,建立了多体系统最优设计数学 模型和算法. 通过双摆系统、曲柄-滑块系统、弹簧/阻尼器-滑块系统3个算例对上述 算法的有效性进行了验证.     

Crack identification method in beam-like structures using changes in experimentally measured frequencies and Particle Swarm Optimization

In this paper, a technique is presented for the detection and localization of an open crack in beam-like structures using experimentally measured natural frequencies and the Particle Swarm Optimization (PSO) method. The technique considers the variation in local flexibility near the crack. The natural frequencies of a cracked beam are determined experimentally and numerically using the Finite Element Method (FEM). The optimization algorithm is programmed in MATLAB. The algorithm is used to estimate the location and severity of a crack by minimizing the differences between measured and calculated frequencies. The method is verified using experimentally measured data on a cantilever steel beam. The Fourier transform is adopted to improve the frequency resolution. The results demonstrate the good accuracy of the proposed technique.