随机激励下滞迟系统的稳态响应闭合解

滞迟系统属于一类典型的强非线性系统,滞迟力不仅取决于系统的瞬时变形,还与变形历程有关.虽然滞迟系统的随机振动问题已被广泛研究,但至今尚未得到滞迟系统随机响应概率密度函数的精确闭合解.本文运用迭代加权残值法获得了高斯白噪声激励下Bouc-Wen滞迟系统稳态响应概率密度函数的近似闭合解.首先,运用等效线性化法求出系统的稳态高斯概率密度函数;然后以此构造权函数,应用加权残值法求得了系统指数多项式形式的非高斯概率密度函数;最后引入迭代的过程,逐步优化权函数,提高计算所得结果的精度.以随机地震激励下钢纤维陶粒混凝土结构的稳态响应作为算例,其中Bouc-Wen模型的参数是基于拟静力学试验数据,并应用最小二乘法辨识获得.与Monte Carlo模拟结果相比,等效线性化法得到的结果精度较差;由加权残值法得到的结果能够表现出非线性特征,但其精度依然无法令人满意;采用迭代加权残值法得到的近似闭合解与Monte Carlo模拟的结果吻合非常好;对于较强随机激励情形,采用渐进迭代加权残值法具有较高的求解效率,所获得的理论解析解具有较高的精度.结果表明,所获得的近似闭合解不仅对于土木工程领域具有重要的实际应用价值,而且还可作为检验其他非线性系统随机响应预测方法的精度的标准.     

随机振动离散分析方法

本文提出了随机振动的离散分析方法,给出了一种可以求瞬态乃至稳态均值和均方响应的递推公式,并证明了它的无条件稳定性。应用该公式可以求出线性和等价线性化的非线性振动系统的精确稳态均值和均方响应。     

分数阶导数阻尼下非线性随机振动结构响应的功率谱密度估计

对于受到由分数阶导数模拟的粘弹性阻尼的非线性随机振动结构,本文给出了一种计算响应的功率谱密度方法。借助标准的随机平均法,首先得到了振动结构随机响应振幅的稳态概率密度。对于原振动结构的非线性项,运用改进的统计线性化方法得到了均方意义下的等价线性振动结构,并求得了其响应的依赖于振幅的条件功率谱密度。综合以上的结果,针对随机振动响应的功率谱密度的估计,通过与数值模拟结果进行验证,从而证明了所提方法的有效性和准确性。     

弹性力学问题的局部Petrov—Galerkin方法

提出了弹性力学平面问题的局部Petrov-Galerkin方法,这是一种真正的无网格方法。这种方法采和移动最小二乘近似函数作为试函数,并且采用移动最小二乘近似函数的权函数作为加权残值法加权函数;同时这种方法只包含中心在所考虑点处的规则局部区域上以及局部边界上的积分,所得系统矩阵是一个带状稀疏矩阵,该方法可以容易推广到求解非线性问题以及非均匀介质的力学问题。还计算了两个弹性力学平面问题的例子,给出了位移和能量的索波列夫模及其相对误差。所得计算结果证明：该方法是一种具有收敛快、精度高、简便有效的通用方法;在工程中具有广阔的应用前景。     

关于加权残值法的充要性问题及其权函数的选择

本文论证了偏微分方程初-边值混合问题的加权残值方程的充要性条件和有关定理。关于充要性条件的讨论也为正确选择解析函数作为权函数,建立充要的加权残值方程提供了理论指导。重点讨论了边界积分方程的充要性。指出了两种满足充要条件的权函数和相应的边界积分方程。     

非线性特征问题计算的扩阶法

本文提出一种可用于求解非线性特征问题的扩阶方法，其基本原理是通过系统矩阵的扩阶使非线性问题线性化．     

非对称非线性随机系统的等价线性化方法及其应用

本文提出了非对称非线性系统在随机干扰下的等价线性化方法以及系统随机反应统计矩的迭代求解方法；在此基础上，利用文献（３）中建立的有损伤结构非对称滞变恢复力模型，研究了结构在主余震作用下的随机反应，最后通过算例比较，验证了本文所提方法的合理性。     

绳系单体系统鲁棒控制实验研究

以交流伺服电机为作动器实现对绳系单体系统的鲁棒控制,建立绳系单体系统的非线性动力学模型,基于平衡点线性化设计μ控制器,针对系统选取合适的权函数并作降阶处理进行在线鲁棒控制。实验结果表明,初始干扰角度在0.4rad范围内,所设计的μ控制器可有效抑制模型参数不确定性及扰动影响,系统有较好的鲁棒性。     

中厚板屈曲的加权残值方法

用加权残值方法分析了矩形中厚板的屈曲问题。试函数和权函数依据短梁函数进行构造。结果良好。     

一种改进的等效线性化方法

提出了一种改进的等效线性化方法.将现有方法中忽略的高阶谐波项作为等效线性方程的外激励,得到非齐次的等效线性化方程,利用谐波平衡法将该方程分解为一系列常微分方程组,用摄动法求解.算例表明,本文方法不仅提高了等效线性化方法的精度,而且对现有方法不能处理的含偶次非线性系统的分析同样有效.     

多自由度柔性结构非线性随机振动响应分析方法

随机等效线性化方法是多自由度结构非线性随机振动分析的有效方法,然而柔性结构隐式的系统方程限制了该方法的应用.本文首先提出了把多自由度柔性结构隐式系统方程显式化的等效非线性系统建立方法,该方法结合模态分析,将系统几何非线性作用等效为模态坐标的高次多项式组合,把多自由度物理系统转化为容易求解的模态系统;在此基础上运用随机等效线性化技术建立柔性结构非线性随机振动响应分析方法.该方法通过引入虚拟激励原理,大幅提高了计算效率,使对多自由柔性结构的非线性随机振动响应分析成为可能.通过算例分析,本文分析结果和精确解与数值模拟解的比较结果表明,本文方法具有较好的计算精度和较高的计算效率,能够应用于实际柔性工程结构的随机振动响应分析.     

非线性滞迟系统的随机振动分析

本文采用非线性滞后函数模型，对于粘弹性系统的随机振动问题，应用等效线性化和方差分析的方法进行了分析研究，给出了白噪声激励下的响应计算解。     

Generalization of Seide’s problem by the regulated stochastic linearization technique

In this paper, the nonlinear random vibration of a uniform beam clamped at both of its ends is investigated by the regulated stochastic linearization technique. A closed system of nonlinear algebraic equations for linearization coefficients is obtained using the frequency–response function matrix. Root mean-square response of maximum deflection of the beam that is obtained from the present technique is subsequently compared with that furnished by the conventional linearization. The numerical results show that the regulated stochastic linearization technique constitutes an excellent alternative to the classical linearization scheme for analyzing responses of the clamped–clamped beam.     

Stochastic optimal control of flexible aircraft taxiing at constant or variable velocity

Active control landing gears are used to alleviate vibration during aircraft taxiing. A nonlinear stochastic dynamics model is established, considering the aircraft body pitch movement and elastic vibration excited by the random runway. The equivalent linearization method is adopted to ensure the model linearity near the balance point, and the Gaussian random process of the runway is generated from the Gaussian white noise using a shape filter. Based on the stochastic optimal control theory, the LQG controller is designed along with weighted quadratic performance index for a better ride comfort, shock absorption, road holding and least energy expenditure. The algebraic Riccati and Lyapunov equations are solved to obtain stationary response while taxiing aircraft at a constant velocity and the differential Riccati and Lyapunov equations are solved to obtain the nonstationary response while taxiing aircraft at a variable velocity. The aircraft dynamic responses are obtained through the runway random process modeled by Monte Carlo method. Simulation results show that active control landing gear can give a better ride comfort, shock absorption and road holding performance no matter whether taxiing is at constant or variable velocity.     

Investigation of Random Response of Rotational Shell When Considering Geometric Nonlinear Behaviour

ＩｎｔｒｏｄｕｃｔｉｏｎＩｎｅｎｇｉｎｅｅｒｉｎｇ,ｔｈｅｎｏｎｌｉｎｅａｒｉｔｙｏｆｓｈｅｌｌｓｔｒｕｃｔｕｒｅｉｓｓｏｍｅｔｉｍｅｓｏｂｖｉｏｕｓ.Ｉｔｉｓｖｅｒｙｄｉｆｆｉｃｕｌｔｔｏｓｏｌｖｅｔｈｅｐｒｏｂｌｅｍｏｆｔｈｅｎｏｎｌｉｎｅａｒｒａｎｄｏｍｖｉｂｒａｔｉｏｎ .Ｉｎｔｈｉｓｐａｐｅｒ,ｗｅｔｒｙｔｏｓｏｌｖｅｉｔｉｎｔｈｅｆｒｅｑｕｅｎｃｙｄｏｍａｉｎｂｙａｎｉｍｐｒｏｖｅｄｓｔａｔｉｓｔｉｃｌｉｎｅａｒｉｚａｔｉｏｎｍｅｔｈｏｄ .Ｗｅｃｏｎｓｉｄｅｒｏｎｌｙｔｈｅｇｅｏｍｅｔｒ…     

A probabilistic linearization method for non-linear systems subjected to additive and multiplicative excitations

A general method to obtain approximate solutions for the random response of non-linear systems subjected to both additive and multiplicative Gaussian white noises is presented. Starting from the concept of linearization, the proposed method of “Probabilistic Linearization” (PL) is based on the replacement of the Fokker–Planck equation of the original non-linear system with an equivalent one relative to a linear system subjected to additive excitation only. By means of the general scheme of the weighted residuals, the unknown coefficients of the equivalent system are determined. Assuming a Gaussian probability density function of the response process and by choosing the weighting functions in a suitable way, the equivalence of the proposed method, called “Gaussian Probabilistic Linearization” (GPL), with the “Gaussian Stochastic Linearization” (GSL) applied to the coefficients of the Itô differential rule is evidenced. In addition, the generalization of the proposed method, called “Generalized Gaussian Probabilistic Linearization” (GGPL), is presented. Numerical applications show as, varying the choice of the weighting functions, it is possible to obtain different linearizations, with a variable degree of accuracy. For the two examples considered, different suitable combinations of the weighting functions lead to different equivalent linear systems, all characterized by the exact solution in terms of variance.     

Random responses of a two-degree-of-freedom structure with strongly nonlinear coupling and parametric interaction

This paper investigates the random responses of a TDOF structure with strongly nonlinear coupling and parametric vibration. With the nonlinear coupling of inertia in the equations of motion of the system being removed by successive elimination, the non-Gaussian moment equation method (NGM) is applied and 69 moment equations are integrated with central cumulative truncation technique. The stochastic central difference-cum-statistical linearization method(SCD-SL) and the digital simulation method(DSM) are also used. A comparison of results by different methods are given and the SCD-SL method is the most efficient method. The project supported by National Natural Science Foundation of China     

迟滞系统受随机激励的响应计算

首先为随机激励设计了具有较高精度的滤波器，把迟滞系统受有色噪声激励的随机振动问题转化为由迟滞系统与滤波器组成的扩阶系统受白噪声激励的随机振动问题，然后详细论述了等效线性化法对此问题的具体求解，着重推导了高斯随机变量联合矩的递推关系和李亚普诺夫方程解法的实现，最后根据数字模拟结果分析了等效线性化法的精度和误差来源，给出了迟滞减振系统参数设计的有关建议。     

考虑参数不确定性的非线性梁随机振动分析

非线性系统的随机振动分析一直是结构动力学领域中的难点,已有一些研究表明基于矩等效的线性化方法在功率谱预测上会得到不恰当的分析结果;另一方面,由于不确定性在实际工程中普遍存在,如果同时考虑非线性和不确定性,更是显著增加了问题难度。本文以具有非线性非理想边界梁为研究对象,基于梁模型的动力学微分方程推导了对应的广义频响函数,并应用Volterra级数理论建立了非线性系统随机振动的谱分析方法,最后,结合蒙特卡洛抽样方法计算了具有参数不确定性非线性梁响应功率谱的均值和方差,讨论了不确定性对结构随机振动响应统计特征的影响。