有约束阻尼的非保守力学系统的稳定性

利用Ｌｙａｐｕｎｏｖ直接法，研究了有势力、陀螺力、Ｒａｙｌｅｉｇｈ阻尼和约束阻尼同时作用的非线性非保守力学系统的稳定性．假设陀螺力依赖某参数ｈ，得到系统渐近稳定的两个定理．     

多自由度非线性系统随机响应的数值算法

本文结合复模态理论，将随机中心差分方法进行推广。给出了一种能直接或等效处理多自由度非线性系统在非平稳随机激励下响应的随机Ｅｕｌｅｒ计算方法。分析适用于经典阻尼和非经典阻尼情况，也适用于非对称系统。     

二类复特征值表达式的适用性研究

对于线性系统，根据其质量、刚度或阻尼等矩阵的性质了解特征值，是十分有意义的问题．对于有阻尼陀螺系统，本文首先通过模态正交性推导了有关矩阵的若干关系式．然后分析了复特征值的两类表达式的适用性，着重讨论了通过一元二次方程研究特征值性质的现行处理方法存在的困难．提出一种确定特征值的补充方法，指出可能存在虚数特征值的系统的性质．算例表明结论正确     

单自由度"加层"减震结构地震作用取值的复模态法

运用复模态方法,以我国现行设计反应谱为基础,对单自由度TMD和“加层”减震结构地震响应及地震作用取值问题进行了系统研究。首先用复模态法将非经典阻尼非对称结构运动方程解耦,然后运用随机振动理论获得结构的动力响应解析式,并建立将结构分解为一系列等效单自由度体系的一般方法,继而利用等效单自由度体系与反应谱的对应关系,确定结构动力响应表达式中各参数的取值,建立结构基于反应谱的设计响应及其等效静态地震作用的设计方法,并给出了算例,从而建立了非经典阻尼非对称结构基于反应谱的地震作用取值的一整套方法。     

关于非保守力学系统的稳定性

关于非保守力学系统的稳定性李俊峰王照林李铁成（清华大学工程力学系，北京１０００８４）１引言力学系统分为保守系统和非保守系统．对保守系统稳定性的研究开展得比较早，研究成果也比较多．非保守系统存在阻尼，线性阻尼有瑞利阻尼和约束阻尼．对于仅有瑞利阻尼作用的...     

陀螺漂移与温度动态过程的试验分析

本文讨论了陀螺仪起动时的热平衡过程，在陀螺漂移和内部温度，特别是温度的变化率之间建立动态数学模型，并且用广义最小二乘（ＧＬＳ）和递推最小二乘（ＩＬＳ）进行辨识。如果陀螺起动过程良好，就可以用补偿方法缩短惯导系统的准备时间。动力调谐陀螺起动过程的重复试验表明，这种方法是可行的     

一类结构的（n－3）重根及其非退化性

基于陀螺模态综合法，从总装阵的块式结构出发，构造性地证明了具有ｎ片桨叶的旋翼型结构陀螺特征值问题存在一系列的（ｎ－３）重特征根，得到了对应的（ｎ－３）个完备的振型．结论进而推广到有阻尼的旋翼型结构．继续研究证明过程表明：结论适用于更广泛的一类具有重复子结构的结构系统，结果表明这类结构几何上的重复性或对称性导致的重根不会引入退化性．不同类型的算例验证了所得到的解析结果．本文还试图说明动力子结构法的定性性质保持特性是值得继续探讨的课题     

一类结构的（n－3）重根及其非退化性

基于陀螺模态综合法，从总装阵的块式结构出发，构造性地证明了具有ｎ片桨叶的旋翼型结构陀螺特征值问题存在一系列的（ｎ－３）重特征根，得到了对应的（ｎ－３）个完备的振型．结论进而推广到有阻尼的旋翼型结构．继续研究证明过程表明：结论适用于更广泛的一类具有重复子结构的结构系统，结果表明这类结构几何上的重复性或对称性导致的重根不会引入退化性．不同类型的算例验证了所得到的解析结果．本文还试图说明动力子结构法的定性性质保持特性是值得继续探讨的课题     

静电悬浮微陀螺的压膜阻尼特性

空气阻尼对静电微陀螺系统的动态特性起着重要的影响。根据流体力学,构建了描述微陀螺内部气体压膜阻尼特性的线性Reynolds方程。将微陀螺内部气膜分成了13个分区,推导了转子在轴向振动、径向振动、径向摆动时的压膜阻尼系数。根据微陀螺的结构参数进行仿真,结果表明:轴向压膜阻尼系数对微陀螺支承系统的动态特性影响最大,而压膜阻尼系数与气体的温度,压强呈线性关系,与振动幅值呈抛物线型关系;在低频段系统呈现阻尼力,而到高频段,系统呈现弹性力。利用Simulink进行了微陀螺的系统建模,得出压膜阻尼系数Cz对PID参数的选取,尤其是Kd参数,起着重要作用,同时对系统的稳定性也有一定的影响。     

光纤陀螺可视化测试系统设计与实现

叙述了光纤陀螺可视化测试系统的设计方案和实现功能。该系统通过VC＋＋6．0中方便简洁的串口通信控件MSComm来实现光纤陀螺的数据采集，并使用技巧的数据存储方法，存储后的数据通过MATLAB7．0开发的数据处理程序进行处理，所有操作均采用模块化设计和可视化方法，方便和简化了复杂的测试过程。实验结果表明整个测试系统具有准确性、方便性等优点。     

The analytical approach for large scale non-classically damped dynamic system

This paper gives a dynamic decoupling approach for the analysis of large scale non-classically damped system, in which the complex variable computations were completely avoided not only in solving for the eigenvalue problem but also in the calculation of the dynamic response. The analytical approaches for undamped gyroscopic system, non-classically damped system, including the damped gyroscopic system were unified. Very interesting and useful theoretical results, practical algorithms were obtained which are applicable to both non-defective and defective systems. recommended by Prof. Yao Zhenhan The project supported by the National Natural Science Foundation of China and the Doctoral Training of Education Committee of China     

EIGENVALUE PROBLEM OF A LARGE SCALE INDEFINITE GYROSCOPIC DYNAMIC SYSTEM

Gyroscopic dynamic system can be introduced to Hamiltonian system.Based on an adjoint symplectic subspace iteration method of Hamiltonian gyroscopic system, an adjoint symplectic subspace iteration method of indefinite Hamiltonian function gy- roscopic system was proposed to solve the eigenvalue problem of indefinite Hamiltonian function gyroscopic system.The character that the eigenvalues of Hamiltonian gyroscopic system are only pure imaginary or zero was used.The eigenvalues that Hamiltonian function is negative can be separated so that the eigenvalue problem of positive definite Hamiltonian function system was presented,and an adjoint symplectic subspace iteration method of positive definite Hamiltonian function system was used to solve the separated eigenvalue problem.Therefore,the eigenvalue problem of indefinite Hamiltonian function gyroscopic system was solved,and two numerical examples were given to demonstrate that the eigensolutions converge exactly.     

Extension of Lagrangian–Hamiltonian mechanics for continuous systems—investigation of dynamics of a one-dimensional internally damped rotor driven through a dissipative coupling

In this paper, the extended Lagrangian formulation for a one-dimensional continuous system with gyroscopic coupling and non-conservative fields has been developed. Using this formulation, the dynamics of an internally and externally damped rotor driven through a dissipative coupling has been studied. The invariance of the extended or so-called umbra-Lagrangian density is obtained through an extension of Noether’s theorem. The rotor shaft is modeled as a Rayleigh beam. The dynamic behavior of the rotor shaft is obtained and validated through simulation studies. Results show an interesting phenomenon of limiting behavior of the rotor shaft with internal damping beyond certain threshold speeds which are obtained theoretically and affirmed by simulations. It is further observed that there is entrainment of whirling speeds at natural frequencies of the rotor shaft primarily depending on the damping ratio.     

Stability boundaries of a spinning rotor with parametrically excited gyroscopic system

Some published papers used Bolotin's method for stability boundaries of spinning rotor with parametrically excited gyroscopic system. However, the original work of the method does not indicate that the method can be used to determine the stability of gyroscopic system. This paper intends to highlight the differences in the results using Bolotin's method. As counter examples, dynamic stability of a special case of the parametrically excited gyroscopic system, a simple gyroscopic rotor under parametric excitation and a rotating Timoshenko shaft subjected to periodic axial forces varying with time are analyzed and discussed by using Bolotin's method and Floquet's method respectively to indicate the differences. The causation of these differences is attributed to the differences in the assumptions of Bolotin's and Floquet's methods as that the assumption of Floquet multipliers in Bolotin's method cannot be satisfied for the gyroscopic system. In this paper it has been shown that the Bolotin's method will result with the enlargement of the instability region for the gyroscopic system, which may contradict the results based upon the Floquet's method.     

接近亏损系统的矩阵摄动法

随着系统参数的变化，带有重频的系统可转变成带有密集频率的系统，反之亦然．本文讨论了亏损系统与接近亏损系统之间的关系．并提出了接近亏损系统的平均移位的摄动方法．算例表明了此方法的有效性．     

The analysis of arbitrarily-damped linear mechanical systems

Summary The analysis of arbitrarily-damped linear mechanical systems is the subject of this paper, the main issue being the analysis of nondecouplable systems. It is well known that decouplable systems occur when the damping matrix happens to be a linear combination of the mass and stiffness matrices. Systems with this type of damping are said to have proportional damping, which nevertheless seldom occurs in practice, but many a damped system is analyzed under the assumption that it is proportionally damped. In fact, this property allows the analyst to study these systems using the same approach as that applicable to their undamped counterparts. In this paper, we show that proportional damping need not be assumed in order to analyze the system at hand with the same approach as used to analyze undamped systems. Moreover, we propose an algorithm to determine the natural frequencies, the damped frequencies and the damping ratios of an n-degree-of-freedom damped system, that does not require the casting of the system into first-order form. In this way, the characteristic equation is derived naturally as a 2n-degree polynomial, computing its roots being then straightforward. Furthermore, we propose a semigraphical method to ease this calculation, which should be attractive to practicing engineers. Received 5 April 1999; accepted for publication 7 May 1999     

Evaluating the Dynamic Load on a High-Speed Railroad Car

The internal dynamic load on a high-speed car following a real rail track with curvature and torsion is evaluated. The centrifugal, gyroscopic, tangential, and Coriolis forces and moments are taken into account. The kinematical parameters were obtained experimentally using an inertial system similar to that used to control space-rocket systems. The Euler-Lagrange equations represented by quaternionic matrices are used to determine the unknown dynamic loads in an explicit analytical form, which makes it possible to evaluate the components of dynamic loads due to the forces and moments acting on the car__________Translated from Prikladnaya Mekhanika, Vol. 41, No. 3, pp. 119–126, March 2005.     

Dynamic stability of a viscoelastic rotating shaft under parametric random excitation

This paper deals with dynamic stability of a viscoelastic rotating shaft subjected to a parametric random axial compressive thrust, by using moment Lyapunov exponents and the largest Lyapunov exponents as indicators. The equation of motion for the shaft is derived, which is a system of gyroscopic stochastic differential equations. The method of stochastic averaging is used to decouple the governing equations into Itô equations, from which the moment Lyapunov exponent is obtained by using mathematical transformations only. The largest Lyapunov exponent is obtained through its relation with moment Lyapunov exponents. The effects of various parameters on the stochastic dynamic stability are discussed. The approximate analytical results are confirmed by Monte Carlo simulation.