非线性单自由度振动系统物理参数的两种辨识方法

本文讨论两种辨识非一单自由度振动系统物理参数的方法，基于描述函数概念的特参数法和由系统时域输入输出信息辨识系统参数的直接时域法。将这两种方法应用于几类非线性背地里自由度振动系统物理参数辨识，并进行了计算机仿真及直接时域法的实验。结果证明了这两种方法的有效性，还提出了对等 参数法的一种改进措施，将 成会考虑在内，以提高辨识精度。     

机械系统中摩擦模型的研究进展

摩擦现象在机械系统中的作用日益突出, 合理地解决机械系统中摩擦环节尤其是非线性摩擦环节的制约问题 已成为当前研究的重点. 由于摩擦的复杂性, 很难从机理上获得其准确唯一的数学模型, 迄今已提出的摩擦模 型有数十种. 鉴于目前机械系统中摩擦建模的发展状况, 首先描述了几种重要的摩擦现象, 如库仑摩擦、黏性 摩擦、Stribeck效应、预滑动摩擦、可变的静态摩擦力和摩擦记忆效应等. 其次, 系统地介绍了几种较为重要的、 常用的摩擦模型, 包括6种静态摩擦模型和7种动态摩擦模型, 并对每一种模型的构成, 特点和适用范围等 进行了较为详细地论述. 比较而言, 静态摩擦模型结构简单, 参数辨识容易, 但是无法描述摩擦的动态特性, 动态摩擦模型能够比较全面的描述摩擦现象, 但结构复杂, 参数辨识难度较大. 再次, 简要概述了摩擦建模 对机械系统动力学行为的影响, 以及在高精度定位系统的控制中的作用. 最后, 针对当前机械系统中摩擦建 模方面存在的一些不足提出了几点展望. 为今后摩擦模型的选用和新摩擦模型的建立提供了参考.     

机械臂控制系统的极限环和混沌运动

本文针对具有关节摩擦的单连杆刚性机械臂控制系统研究了运动轨迹的极限环和混沌现象。利用Ｈａｍｉｌｔｏｎ原理建立了机械臂的动力学模型，考虑了不同的摩擦模型，针对具有库仑摩擦和粘性摩擦的机械臂控制系统，建立了系统非线性部分的描述函数，并且证明了该系统存在稳定的极限环。利用Ｌｙａｐｕｎｏｖ线性化方法和数值仿真研究了系统的混沌现象。     

两自由度的Burridge-Knopoff模型的一种近似分析方法

Burridge-Knopoff模型是速度驱动的多质量的质量弹簧系统.它是用来进行地震机理研究的一种摩擦动力系统的模型.本文考查了具有两个自由度的Burridge-Knopoff模型的摩擦激振问题.摩擦的不光滑性给系统的求解带来了很大的困难.又系统带有两个摩擦接触面,运动情况更加复杂.本文通过对摩擦力取平均的方法,得到了系统在各个运动形式下的通解,采用半解析的方法对此两自由度的系统进行了研究.通过以上方法,给出了一种周期运动的具体运动形式以及位移和速度的时程关系;并且发现在不同驱动速度的情况下,随着驱动速度的增大,系统的运动形式存在简单和复杂交替出现的现象,并给出了不同系统参数下的分岔图.     

超声速飞行器壁板非线性颤振响应分析的时域法与频域法对比研究

为考查基于假设模态法在时域中开展壁板非线性颤振分析的可行性,在相同的参数下,分别采用时域方法和频域方法研究了超声速飞行器壁板的非线性颤振响应,并从壁板的颤振幅值、颤振频率和颤振型态三个方面对时域和频域分析结果的一致性作了较详细的比较。首先,基于von Karman应变－位移关系和Mindlin板理论建立考虑几何非线性的壁板力学模型,应用一阶活塞理论分析壁板上单面承受的超声速准定常气动力,基于虚功原理和有限单元法推导壁板的运动微分方程。然后,用壁板的线性固有模态作为假设模态,减缩系统的自由度而得到降阶模型。采用四阶龙格-库塔法对降阶模型作时域数值积分,得到壁板的非线性颤振响应。另一方面,假设壁板的极限环颤振为简谐振荡,可对壁板的非线性刚度作等效线性化处理,进而在频域中直接在有限元（未降阶）模型的基础上分析壁板的颤振幅值、颤振频率和颤振型态。数值分析表明,当极限环颤振为简谐振荡时,时域方法和频域方法的计算结果符合一致。本文最后讨论了时域法和频域法应用在壁板非线性颤振分析中各自的优点和局限性。     

界面连接刚度参数辨识的子结构分析法

以试验模态参数为基础,提出一种通过特征方程反问题辨识子结构界面连接刚度参数的子结构分析法。新方法以子结构动柔度矩阵特征方程为基础,建立求解界面结点内力和位移的方程,从而由子结构内部结点可测自由度上的位移用广义逆理论估计界面结点内力和位移。并通过迭代修正内部结点可测自由度上的试验值,以提高界面内力和位移的估计精度。最后通过连接子结构刚度矩阵建立的平衡方程求解相应的刚度参数。文中以太阳电池阵板间铰链副刚度参数辨识为例,将铰链副简化为两端结点各有6个自由度的弹簧连接元,考虑到自由度之间的耦合,推导了连接元的刚度矩阵。用上述方法辨识了铰链副6个自由度的刚度参数,得到满意的辨识结果。     

带有摩擦耗能元件的框架结构动力分析

本文提出粘性屈服模型来模拟摩擦耗能元件的力-速度关系,该模型是连续变化的,克服了库仑摩擦模型不连续导致数值计算复杂的缺点,在进行摩擦耗能体系的动力分析中,采用缩减自由度技术,并作适当的变换,则带有摩擦耗能元件体系的动力分析归结为求解微分代数方程,本文采用增量型Rosenbrock二级三阶半隐式Runge-Kutta法求解该方程,以考虑框架和支撑的材料和几何非线性。对带有摩擦耗能元件的钢框架进行了弹塑性动力分析,研究了支撑刚度与结构层刚度的比值、摩擦力的大小以及地震波类型等参数对体系的影响。     

平流层飞艇气动参数辨识

进入21世纪以来，随着科技的飞速发展，世界上掀起了研究和开发平流层平台的热潮。飞艇作为平流层平台可以实现无线通信、空间观测、大气测量以及军事侦查等目的。本文首先将飞艇所受的气动力分成由于来流速度产生的定常气动力和飞艇转动引起的非定常气动力两部分，通过理论分析建立了飞艇的气动力模型，从而得到需要辨识的气动参数。其次建立了以浮心为原点的六自由度非线性动力学模型和一种基于混合遗传算法的气动力系数辨识方法——混合遗传算法（遗传算法＋单纯型法）与极大似然法相结合的方法，并利用该方法对飞艇的气动参数进行辨识。通过仿真结果验证了该方法实用性和有效性。最后通过对气动参数的准确值与辨识值的分析比较，得出各个参数对飞艇运动性能的影响情况。     

流体阻尼器中粘性发热的反馈作用与热平衡研究

主要针对长阻尼孔形式下的流体阻尼器进行分析,在三参数模型的基础上研究了流体粘性发热对流体阻尼力的反馈作用,从而建立了含热能转换与热交换的阻尼器的动力学模型,同时对系统的热平衡状态进行了分析。最后通过数值分析对该时变系统从时域和频域上讨论了粘性发热对隔振效果的影响,发现温度变化对共振频率的漂移及幅值大小的影响较大。     

基于机器学习的动力学环境预测方法

为了研究建立同一结构在两个不同系统中振动响应之间的映射关系模型的基本问题,以两种边界条件组成的两个系统为例,从其动力学方程出发,建立了基于时域、频域描述的映射关系的力学模型.为求解两个系统的映射关系模型,引入以统计学习理论为基础的机器学习方法——支持向量机法,借助于决策函数可以从一种边界条件预测同一结构在另一种边界条件下结构的响应,并通过实验证明了该方法的有效性.     

Digital image processing for non-linear system identification

Emerging digital image processing techniques demonstrate their potential applications in engineering mechanics, particularly in the area of system identification involving non-linear characteristics of mechanical and structural systems. The objective of this study is to demonstrate the proof-of-concept that the techniques permit the identification non-intrusively and remotely. First, the efficacy of the digital image processing method is shown by identifying the friction behavior between two solids that are assumed to be governed by the Coulomb friction model. The inverse analysis is carried out to validate the proposed method of identifying model parameters. Studies further illustrate that the digital imaging procedure and inverse analysis algorithms developed for the friction problem can be extended for identification of non-linear mechanical and structural characteristics. One illustration utilizes the second example, where relative motion between a model structure and a shaking table is measured by digitally processing the analogue image provided by a video tape recorded during a shaking table test of a model structure base isolated by a hybrid isolation device consisting of friction and elastomeric components. Third, constitutive relationship for a non-linear elastomeric membrane is identified by digitally processing images of its deformed states under tension. The relationship is postulated to follow the Mooney-Rivlin function. Schemes developed are verified with iterative non-linear finite-element program that is valid in the finite deformation range. Emerging cost-effective hardware and software systems for high-performance data acquisition and processing are quite promising to the implementation of the techniques by removing most, if not all, of its existing limitations.     

Analytical parametric study of bi-linear hysteretic model of dry friction under harmonic,impulse and random excitations

Hysteretic behavior due to some nonlinear sources is a common phenomenon in many dynamical systems. One of the sources of this behavior in mechanical systems is dry friction. Dry friction in bolted or riveted joints of mechanical structures makes their dynamic behavior hysteretic. Bi-linear hysteresis is one of the models that can be used to study these systems which is used in this paper. A SDOF system containing a bi-linear hysteretic element called Jenkins element under harmonic, impulse and random excitations is considered. For all three types of excitations, the effects of system and excitation parameters on the defined equivalent system parameters and the response specifications are studied. Harmonic balance method is employed for harmonic excitation studies, and optimum friction threshold for minimizing response amplitude is obtained versus other system parameters and response amplitude. Energy balance method is used for impulse excitation through which the desired decaying ratio can be achieved by tuning the friction threshold, depending on stiffness ratio. System under random excitation is investigated by equivalent linearization technique in two steps. At the first step, equivalent properties are obtained versus instantaneous amplitude of response. In this step, the paper contains the parametric study of system in which the variations of equivalent parameters are described when physical parameters of system or input intensity vary. Overall variance of system response is determined in the second step, and optimum sliding threshold is obtained to have minimum overall variance of system response.     

Analytical investigation of an SDOF building structure equipped with a friction damper

The purpose of this study is to investigate analytically a single-degree-of-freedom (SDOF) building structure equipped with a friction damper for assessing its vibration control effect. Friction dampers are installed between stories to reduce inter-story displacements of building structures subjected to external loading. They are in general regarded to generate damping forces characterized by Coulomb damping, of which the directions are opposite to the inter-story velocities of building structures. Hence, the building structure model with friction dampers can be represented by a mass-spring-viscous-Coulomb damping system. The building response reduction as a result of damper installation can be provided by observing the damping ratio rather than the friction force contributed by the dampers. Since a large friction damper force is required to attenuate the response of the building due to strong excitation, friction force ratio is directly related to building response reduction, which is the friction force of the damper versus external force. Therefore, damping and friction force ratios are key parameters, playing a main role in selecting an optimal friction damper, which satisfies target response reduction. This study first identifies an SDOF building structure installed with a friction damper for free vibration with initial conditions. A?closed-form expression of normalized displacement is derived in terms of friction force ratio in the time domain. Peak and valley of displacements are also found and then the time when the structure stops is derived with recursive interval number. This study is extended to identify steady-state vibration of the structure by deriving closed-form solution in case of resonance in terms of friction force ratio. Then, the dissipated energy balance is identified for both free and steady-state vibrations. Finally, equivalent viscous damping ratios are derived by using friction force ratio based on dissipated energy balance equation. The derived equations in terms of viscous damping ratio and friction force ratio can provide insight to design a friction damper for reducing structural displacement under external loadings.     

A comprehensive study on the behavior of a rigid block on an oscillating ground with friction,elastic and viscous forces

This paper investigates the behavior of a non-linear mechanical model where a block is driven by an oscillating ground through Coulomb friction, a linear viscous damper and a linear spring. The governing equation is solved analytically for different partial configurations: friction only, friction with viscous damping, friction with a linear restoring force, and for the complete model. Using dimensionless groups, the analysis of the block motion provides a comprehensive set of information on the motion regime (stick, stick-slip or permanent sliding), on the dominant energies or forces, on the resonance and on the amplification of the ground oscillation by the system. The limit between the stick-slip regime and the permanent slipping regime is found either analytically or numerically. It is also shown that there exists a set of parameters for which the friction force, the viscous dissipative force and the elastic restoring force are equal.     

The effects of Coulomb friction on the performance of centrifugal pendulum vibration absorbers

We investigate analytically and experimentally the effects of Coulomb friction on the performance of centrifugal pendulum vibration absorbers (CPVAs), which are used to reduce torsional vibrations in rotating machinery. The analysis is based on perturbation methods applied to the nonlinear equations of motion for a rotor subjected to an engine order applied torque and equipped with a circular path CPVA with viscous and Coulomb damping. The experimental work is based on quantifying parameters for the damping model using free vibration measurements with a viscous and Coulomb damping identification scheme that is enhanced to better handle measurement noise, and running tests for steady-state operation under a range of loading conditions. The level of Coulomb damping is varied by adjusting the friction of the absorber connection bearing. Good agreement is found between the analytical predictions and the experimental data. It is shown that the absorber sticks up to a level of excitation that allows it to release, after which the Coulomb damping acts in the expected manner, resulting in lowered response amplitudes. The results obtained are of general use in assessing absorber performance when dry friction is present in absorber suspensions.     

基于LuGre摩擦模型的接触约束法旋转柔性梁斜碰撞研究

基于接触约束法和LuGre摩擦模型对在重力场作用下作大范围旋转运动的柔性梁系统和斜坡发生含摩擦斜碰撞的动力学问题进行研究. 首先运用刚柔耦合的多体系统动力学理论对大范围运动的柔性梁进行离散化和动力学建模, 在碰撞时采用冲量动量法求出跳跃速度, 其次在法向上引入接触约束求解出碰撞力, 在切向上采用LuGre摩擦模型分两种方式求解摩擦力, 第一种是在滑动时摩擦力由摩擦系数和碰撞力计算得出, 黏滞状态下引入切向约束计算拉格朗日乘子反应实际摩擦力, 根据黏滞/滑动切换判断计算出碰撞过程摩擦力(与Coulomb摩擦模型计算摩擦力一致); 第二种根据LuGre摩擦模型摩擦系数和法向碰撞力计算其摩擦力, 从而在碰撞时无需黏滞/滑动切换, 采用相同的摩擦力计算公式. 通过与Coulomb摩擦模型对比发现, LuGre摩擦模型描述碰撞切向摩擦过程更精确, LuGre摩擦模型黏滞时建立约束方程和碰撞采用统一的摩擦力公式这两种建模方式描述的斜碰撞动力学特性没有区别, 进而说明采用法向接触约束和LuGre摩擦模型具有满足碰撞非嵌入情况、避免黏滞/滑动切换、描述摩擦力相对准确的优势.      

Equivalent linearizations for practical hysteretic systems

Experimental testing of a friction damped base isolation system has indicated a need for a new model of friction damping and for an appropriate equivalent linearization technique. The model for the damping adopted is a combination of viscous damping, constant Coulomb friction and linear Coulomb friction.This model is incorporated into the equation of motion for a single-degree-of-freedom system and the exact solutions are given for free vibrations and for steady-state vibrations excited by a harmonic force. The exact solution is taken as a basis for an equivalent linearization technique that can be used in conjunction with conventional design spectra for a practical design of such a system.