含有分叉的受控多体系统传递矩阵法

多体系统传递矩阵法是解决受控多体系统动力学问题的有效方法,针对含有分叉的受控多体系统动力学问题,分别建立了控制激励元件、控制反馈元件及其含有分叉的受控多体系统总体传递矩阵．实例计算了无控和受控多体系统的运动响应与牛顿欧拉方法比较,计算表明了受控多体系统传递矩阵法解决分叉控制系统运动的有效性．     

多管火箭射击精度仿真试验新方法

该文提出了多管火箭射击精度的仿真试验新思路,构造了射击精度仿真试验的基本框架。对多管火箭射击精度仿真试验的研究内容、研究方法和技术途径进行了论述,表明系统仿真模型的校核、验证和确认是关键。提出应用多体系统传递矩阵法,建立刚柔耦合多管火箭动力学模型,通过建立增广特征矢量,获得其正交性条件,实现对多管火箭振动特性和动力响应的精确分析的仿真算法。结合简易控制和弹道理论,建立多管火箭射击精度仿真系统。应用最大熵方法,形成了多管火箭射击精度仿真试验的新方法。     

非完整约束多体系统时间离散变分积分法

基于连续Galerkin方法,给出非完整约束下多体系统时间离散的变分数值积分方法.首先对非完整多体系统Hamilton正则方程的弱形式进行时间离散,得到变分积分公式,然后讨论该积分方法对能量及约束的保持,最后以蛇板为例对该方法进行数值验证和比较.     

远程多管火箭动力学研究

对某远程多管火箭发射与控制动力学进行了深入的理论、计算和试验研究,建立了某远程多管火箭刚弹耦合的多体系统发射动力学模型和发射与控制动力学方程．应用多体系统传递矩阵法,实现了对刚柔耦合远程多管火箭振动特性的计算;构造了远程多管火箭增广特征矢量及其正交性条件,实现了对该远程多管火箭动力响应的精确分析．对某远程多管火箭武器振动特性和动力响应的仿真结果得到了试验验证．为提高远程多管火箭密集度和减少试验用弹量奠定了基础。     

《结构动力学》中多频激励多自由度系统稳态解的新方法

本文建立了一种多频激励下多自由度系统的特征值和稳态解的解析求解新方法.基于叠加原理,首先将稳态响应根据激励频率数量展开成多个简谐响应的叠加;其次,根据简谐平衡原理,将弹簧力、激励荷载以及惯性力分解成同样个数的对应荷载叠加;再次,根据达朗贝尔原理建立弹簧和质点的动态平衡方程;最后,根据传递矩阵法进行求解.通过4自由度系统...     

离散时间分数阶多自主体系统的时延一致性

复杂工作环境中,许多自然现象的个体动力学特性用整数阶方程不能描述,只能用非整数阶（分数阶）动力学来描述个体的运动行为. 本文假设多自主体系统内部连接组成有向加权网络,个体的动态特性应用分数阶动力学方程描述,个体之间数据传输存在通信时延. 应用分数阶系统的Laplace变换和频域理论,研究了离散时间的分数阶多自主体系统的渐近一致性. 应用Hermit-Biehler 定理,研究了具有样本时延的分数阶多自主体系统的运动一致性,得到保证系统稳定的时延的上界阈值. 最后应用一个实例对结论进行了验证.     

多体系统动力学数值解法

多体系统动力学研究的主要内容动力学建模与数值解法是多体系统动力学研究的主要内容之一。对多体系统动力学方程及其动力学数值解法的研究成果进行了较为全面的阐述。多体系统动力学及动力学方程进行了简单的归纳和总结,多体系统动力学数值求解,特别是刚柔耦合多体系统微分／代数方程的数值解法等研究热点进行了详细的阐述,并简要展望了多体系统动力学数值解法今后的发展趋势,为多体系统动力学计算机仿真奠定了基础。     

基于CORBA的多体系统动力学分布式仿真

基于多体系统动力学与运动学的机械系统计算机辅助分析(CAA)已成为该领域计算机辅助工程(CAE)的核心内容。该文分析了多体系统动力学方程建立及求解方法，结合CORBA技术、数值分析方法、OpeaGL图形技术，开发了基于CORBA的多体系统动力学分布式仿真系统，实现了分布式环境下的多体系统动力学的数值分析与仿真。     

多体系统多点碰撞接触问题的数值求解方法

多体系统多点接触碰撞问题可以归结为一个将系统的动力学方程与并协性约束方程相结合的问题.针对这样一个含并协性条件的混合方程组,建立了基于 LCP 格式的包含碰撞/接触问题的多刚体系统动力学分析框架,提出了一种基于步长评价准则的变时间步长的数值求解策略,实现了无摩擦情况下多刚体系统多点接触碰撞问题的数值算法.最后给出了数值算例,验证了算法的有效性.     

具有双面约束单点摩擦多体系统的数值计算方法

研究了一类具有双面约束单点摩擦的单自由度多体系统动力学方程的算法问题.首先给出了系统的动力学方程,该方程具有很强的非光滑性,不能应用已有的一些光滑系统的数值方法研究系统的动力学特性.因此,本文利用方程的特点和所求变量的物理含义,给出了一种简便的数值计算方法.该方法的计算效率和精度与迭代法相比均较高.     

Transfer matrix method for linear multibody system

A new method for linear hybrid multibody system dynamics is proposed in this paper. This method, named as transfer matrix method of linear multibody system (MSTMM), expands the advantages of the traditional transfer matrix method (TMM). The concepts of augmented eigenvector and equation of motion of linear hybrid multibody system are presented at first to find the orthogonality and to analyze the responses of the hybrid multibody system using modal method. If using this method, the global dynamics equation is not needed in the study of linear hybrid multibody system dynamics. The MSTMM has a small size of matrix and higher computational speed, and can be applied to linear multi-rigid-body system dynamics, linear multi-flexible-body system dynamics and linear hybrid multibody system dynamics. This method is simple, straightforward, practical, and provides a powerful tool for the study on linear hybrid multibody system dynamics. This method can be used in the following: (1) Solve the eigenvalue problem of linear hybrid multibody systems. (2) Obtain the orthogonality of eigenvectors of linear hybrid multibody systems. (3) Realize the accurate analysis of the dynamics response of linear hybrid multibody systems. (4) Find the connected parameters between bodies used in the computation of linear hybrid multibody systems. A practical engineering system is taken as an example of linear multi-rigid-flexible-body system, the dynamics model, the transfer equations and transfer matrices of various bodies and hinges; the overall transfer equation and overall transfer matrix of the system are developed. Numerical example shows that the results of the vibration characteristics and the response of the hybrid multibody system received by MSTMM and by experiment have good agreements. These validate the proposed method.     

基于Hermite 插值的多体系统动力学离散变分方法

针对多体系统动力学数值仿真问题,研究基于Hermite插值的离散变分方法.首先对广义坐标和广义速度进行Hermite插值,结合Gauss数值积分方法,利用Hamilton原理和离散力学变分原理,建立了含已知导数信息和含未知导数信息的Hermite插值离散变分数学模型,求解得到精确度较高的动力学仿真结果.该方法可以在步长较大时精确保持约束方程,并保持系统总能量在一定范围内有界变化,适用于长时间仿真情况.     

Geometric properties of projective constraint violation stabilization method for generally constrained multibody systems on manifolds

During numerical forward dynamics of constrained multibody systems, a numerical violation of system kinematical constraints is the important issue that has to be properly treated. In this paper, the stabilized time-integration procedure, whose constraint stabilization step is based on the projection of integration results to underlying constraint manifold via post-integration correction of the selected coordinates is discussed. A selection of the coordinates is based on the optimization algorithm for coordinates partitioning. After discussing geometric background of the optimization algorithm, new formulae for optimized partitioning of the generalized coordinates are derived. Beside in the framework of the proposed stabilization algorithm, the new formulae can be used for other integration applications where coordinates partitioning is needed. Holonomic and non-holonomic systems are analyzed and optimal partitioning at the position and velocity level are considered further. By comparing the proposed stabilization method to other projective algorithms reported in the literature, the geometric and stabilization issues of the method are addressed. A numerical example that illustrates application of the method to constraint violation stabilization of non-holonomic multibody system is reported. An erratum to this article can be found at     

Discrete time transfer matrix method for dynamics analysis of complex weapon systems

Efficient, precise dynamic modeling and analysis for complex weapon systems have become more and more important in their dynamic design and performance optimizing. As a new method developed in recent years, the discrete time transfer matrix method of multibody system is highly efficient for multibody system dynamics. In this paper, taking a shipboard gun system as an example, by deducing some new transfer equations of elements, the discrete time transfer matrix method of multibody sys- tem is used to solve ...     

Discrete Time Transfer Matrix Method for Multibody System Dynamics

A new method for multibody system dynamics is proposed in this paper. This method, named as discrete time transfer matrix method of multibody system (MS-DT-TMM), combines and expands the advantages of the transfer matrix method (TMM), transfer matrix method of vibration of multibody system (MS-TMM), discrete time transfer matrix method (DT-TMM) and the numerical integration procedure. It does not need the global dynamics equations for the study of multibody system dynamics. It has the modeling flexibility and a small size of matrices, and can be applied to a wide range of problems including multi-rigid-body system dynamics and multi-flexible-body system dynamics. This method is simple, straightforward, practical, and provides a powerful tool for the study of multibody system dynamics. Formulations of the method as well as some numerical examples of multi-rigid-body system dynamics and multi-flexible-body system dynamics to validate the method are given.     

基于修订矩阵的最小二乘法多传感器融合障碍物位置估计

在障碍物位置检测时,由于传感器测量误差等不确定因素的存在,希望通过多传感器融合降低不确定性使得位置估计值更为可靠.提出了一种基于修订矩阵的最小二乘法多传感器融合估计新方法.根据红外传感器得出的先验信息建立修订矩阵,再由最小二乘法的原理得出线性可信度加权方程.分别对加入和不加入修订矩阵进行仿真和"未来之星"移动机器人实验...     

含干摩擦多体系统Lagrange方程的数值算法

利用第一类Lagrange方程建立了固定约束面含干摩擦的多体系统动力学方程,将摩擦力的广义力用矩阵形式描述．利用增广法。将微分-代数方程转换成常微分方程,并用矩阵形式给出,提高了计算效率．最后用算例说明该方法的有效性．     

通用几何约束系统统一建模研究

在几何约束和几何实体的基本约束和欧拉参数表达的基础上,研究了通用几何约束系统的统一建模问题。通过对三维几何实体姿态约束和位置约束解耦性的分析,抽象出球实体、盒体和球盒体三种基本几何实体表达空间几何实体,并以基本约束的组合表达几何约束,形成几何约束模型特有的层次结构;并以有向图管理几何约束系统,可以清晰地反映姿态约束和位置约束的解耦性,实现约束系统的细粒度分解,得到规模更小的求解序列,实现高效求解。方法实现于原型系统WhutVAS中。     

Motion correction based on an appropriate system matrix for statistical reconstruction of respiratory-correlated PET acquisitions

Respiratory motion correction in positron emission tomography (PET) seeks to incorporate motion information into an image reconstruction algorithm by using the full counting statistics of an acquisition to generate a single, motion-free volume. Here, we present a motion-incorporated ordered subsets expectation maximization (MOSEM) reconstruction based on a device-dedicated tomographic projector in which each matrix element is calculated directly from the voxels’ Cartesian coordinates alone. The motion is corrected by updating this projector as a function of the respiratory level. The performance of the reconstruction method was investigated with three datasets: two simulations of a transaxially or axially moving lesion on a patient acquisition and a third acquisition of a moving sphere. After the 16th sub-iteration, the normalized mean square error (NMSE, with a motionless acquisition as reference) was 0.20 for the non-corrected (ungated) image and 0.01 for the MOSEM image with transaxial motion simulation. Likewise, NMSE was 0.30 for the ungated image and 0.03 for MOSEM image with axial motion simulation. For the phantom, ungated reconstruction yielded an error of 0.78, whereas MOSEM yielded 0.43. The error reduction resulted from enhancement and reduced spreading of the moving uptake. Our results show that MOSEM reconstruction yields motion-corrected images which are similar to motionless reference images.