武器结构-机构耦合系统的最优化设计

本文提出了具有结构，机构耦合形式的自动武器系统的最优化设计问题，建立了这种武器系统在射击载荷作用下的ＮＬＰ模型，针对武器系统的非线性耦合特性，提出了状态和设计敏度分析的混合预测校正方法，建立的ＮＬＰ问题用改进的ＳＬＰ方法求解，通过对一简单的后退式武器后座力的最小化设计说明本文方法有是有效的。     

有杆抽油系统动态特性的计算机仿真

本文建立了有杆抽油系统动态特性仿真的综合数学模型．即应用数值积分法建立转子运动规律的仿真模型和应用差分法建立抽油杆柱纵向振动的仿真模型。本文提出了一种叠代方法较好地解决了两子系统之间相互耦合的问题，给出了一种便于应用的井下边界条件的仿真方法。     

求解三维弹性力学问题的快速耦合方法

将多种数值方法耦合,充分利用各种方法的优点建立新的数值方法,是求解三维复杂问题的有效途径之一．本文将无单元Galerkin (Element-Free Galerkin, EFG)方法、有限元法和维数分裂法耦合,提出了求解三维弹性力学问题的快速耦合方法(Fast Hybrid Method, FHM)．将三维弹性力学问题分裂为若干个二维平面问题,对于每个二维问题采用罚函数法施加边界条件,并推导其相应的积分弱形式,引入Shepard基函数的移动最小二乘法建立形函数,进而推导二维平面问题的离散方程．第三个方向上采用有限元法将这些二维离散方程进行耦合,可以得到原三维弹性力学问题的快速耦合方法数值解的求解公式．通过数值算例验证了本文快速耦合方法求解三维弹性力学问题的收敛性,将数值解与解析解对比,说明了本文方法求解三维弹性力学问题的有效性．     

弹性与弹塑性问题的有限元与边界元耦合解法

本文提出了一种新的弹性与弹塑性问题的对称耦合解法，根据分区广义变分原理，直接导出问题的求解方程式。通过典型算例，验证了该方法的有效性，本文建议的方法怀超单元形式的耦合法相比，在理论上比较直接，在计算上更为经济。     

考虑风-结构-土耦合作用时高层建筑顺风向风振响应分析

本文综合考虑了风-结构-土的耦合作用对高层建筑顺风向风振响应的影响，研究了在各种参数下高层建筑风振响应的特性。由于在风-结构-土耦合作用问题的整个体系的控制方程中，既有时域中的耦合关系，又有频域中的耦合关系，本文提出采用傅立叶变换-时频迭代法来进行求解，较好地解决了用普通的方法难以解决的问题。最后采用数值计算的方法比较了考虑风-结构-土的耦合作用和仅考虑土-结构相互作用以及刚性基础的结构位移响应及加速度响应。     

管道流固耦合振动的行波方法研究

应用波动方法分析载流管道流固耦合振动问题。采用直梁模型，推导了管道流固耦合系统的轴向、横向波导方程及平面管系的坐标转换矩阵，通过节点位移连续和力平衡条件建立了耦合系统的散射模型。最终分析了两种耦合对载流管道振动的影响机理及流速变化对管道振动稳定性的影响。数值算例表明本文方法的正确性及有效性。     

考虑固体域几何非线性的固液耦合系统瞬态有限元分析

本文基于理想可压缩流体压力传输方程及增量型ＴｏｔａＩＬａｇｒａｎｇｉａｎ列式，建立了考虑固体域几何非线性的固液耦合系统有限元方程，并开展了非线性分析工作。本文的方法可用于流体域远大于固体域，从而可仅仅研究固体域非线性响应的情况。由于流体域每个节点仅有一个未知量（压力），故流体域的计算规模得以大大减缩。同时，因为本文方法仅需对固体域进行非线性分析，故显著地简化了固液耦合非线性问题的求解工作。本文的方法亦可用于三维分析。     

风与柔性结构流固耦合作用的预处理方法研究

针对强耦合方法求解风与柔性结构流固耦合作用时,大量计算资源都耗费在对强耦合方程求解中这一弊端,本文研究了强耦合方程的预处理求解方法。在风与柔性结构流固耦合作用的强耦合整体方程的基础上,将时空离散和线性化后的类似结构方程看成是鞍点问题,首先推导得到了类似结构方程的预处理矩阵;再基于此推导出了强耦合整体方程的预处理矩阵。首先采用预处理方法对经典二维流固耦合问题进行了计算,验证了提出的预处理矩阵的正确性;然后对风与三维膜结构的流固耦合作用进行了分析,评估了所提出预处理方法的相关计算参数。计算结果表明,所提出的预处理方法可使强耦合整体方程的求解在计算精度和计算效率上都得到较大提升,证明本文提出的预处理方法适用于风与柔性结构的流固耦合分析。     

树木在风中摇曳的流固耦合数值模拟方法探索

树木在风中摇曳是一个流固耦合问题,但树的结构复杂,无法直接用已有的流固耦合数值方法来模拟.本文提出一种基于虚拟耦合面的流固耦合方法,该方法用一个虚拟的连续曲面把树冠包裹起来,在这个曲面上建立流固耦合关系,并将虚拟曲面上计算得到的风荷载作为树木结构的外力进行加载.虚拟耦合面本身不妨碍树木枝条的运动,且能避免在每个枝条、树...     

无网格Galerkin法与非协调元方法的耦合

无网格Galerkin法(EFGM)处理不可压缩问题时不存在自锁现象，有限元方法(FEM)也常被用来与其耦合以方便地施加边界条件和提高计算效率。在有限元方法中使用等参元，EFGM与FEM的耦合方法在处理不可压缩问题时仍然存在自锁现象。本文在有限元方法中，采用非协调元，将无网格kGalerkin法与非协调元耦合，保留了耦合方法的优点，且避免了求解不可压缩问题时的自锁现象。算例显示本文方法在分析平面应变不可压缩问题时能得到合理的结果。     

A Hybrid Nonlinear Programming Method for Design Optimization*

ABSTRACT

Solutions to engineering design problems formulated as nonlinear programming (NLP) problems usually require the use of more than one optimization technique. Moreover, the interaction between the user (analysis/synthesis) program and the NLP system can lead to interface, scaling, or convergence problems. An NLP solution system is presented that seeks to solve these problems by providing a programming system to ease the user-system interface. A simple set of rules is used to select an optimization technique or to switch from one technique to another in an attempt to detect, diagnose, and solve some potential problems. Numerical examples involving finite element based optimal design of space trusses and rotor bearing systems are used to illustrate the applicability of the proposed methodology.     

Optimal control of attitude for coupled-rigid-body spacecraft via Chebyshev-Gauss pseudospectral method

The attitude optimal control problem(OCP) of a two-rigid-body spacecraft with two rigid bodies coupled by a ball-in-socket joint is considered. Based on conservation of angular momentum of the system without the external torque, a dynamic equation of three-dimensional attitude motion of the system is formulated. The attitude motion planning problem of the coupled-rigid-body spacecraft can be converted to a discrete nonlinear programming(NLP) problem using the Chebyshev-Gauss pseudospectral method(CGPM). Solutions of the NLP problem can be obtained using the sequential quadratic programming(SQP) algorithm. Since the collocation points of the CGPM are Chebyshev-Gauss(CG) points, the integration of cost function can be approximated by the Clenshaw-Curtis quadrature, and the corresponding quadrature weights can be calculated efficiently using the fast Fourier transform(FFT). To improve computational efficiency and numerical stability, the barycentric Lagrange interpolation is presented to substitute for the classic Lagrange interpolation in the approximation of state and control variables. Furthermore, numerical float errors of the state differential matrix and barycentric weights can be alleviated using trigonometric identity especially when the number of CG points is large. A simple yet efficient method is used to avoid sensitivity to the initial values for the SQP algorithm using a layered optimization strategy from a feasible solution to an optimal solution. Effectiveness of the proposed algorithm is perfect for attitude motion planning of a two-rigid-body spacecraft coupled by a ball-in-socket joint through numerical simulation.     

具有环形缓冲簧的武器系统的动力分析与优化

本文对带有预压环形缓冲簧的自动武器系统进行了模型化,提出了系统动力方程的分块分段求解方法,建立并用改进算法求解了以后坐力为最小化目标的非线性规划问题。文末给出了某火炮在连发射击条件下的分析与优化结果。     

The optimal distributed filtering for the coupled systems with random delay

The interactions between subsystems are important for large-scale systems, which render the whole system highly nonlinear. In this paper, we address the optimal distributed filtering problem for a kind of local strongly coupled systems. The coupled systems interact by communication in which there are random delays and data dropouts. First, we conduct a strongly coupled system with communication between the nodes. Applying the standard Kalman filter design procedures to such systems is difficult because of transmission delay and intermittent communication. Then, we use the stochastic theory and state augmentation technique for the proposed systems. We present the optimal filtering problem in terms of the full system dynamics. Finally, the numerical simulations show the effectiveness of the filtering method proposed.     

Application of Modelica/MWorks on modeling,simulation and optimization for electro-hydraulic servo valve system

Electro-hydraulic servo valve is a typical complicated multi-domain system constituted by mechanical, electric, hydraulic and magnetic components, which is widely used in electro-hydraulic servo systems such as construction machinery, heavy equipment, weapon and so forth. The traditional method of modeling and simulation of servo valve is based on block diagram or signal flow, which cannot describe the servo valve system from components level nor be used in modeling and simulation of overall servo systems. In the procedure of traditional method, computational causality must be involved in modeling of servo valve, which is inconvenient to execute modification on components or parameters. Modelica is an object-oriented modeling language which is suited for large, complex, heterogeneous and multi-domain systems. The key features of Modelica are multi-domain, object-oriented and non-causal, which are suitable for modeling of servo valve and make the model readable, reusable, and easy to modify. The simulation results show similar curves with traditional method. This new servo valve modeling and simulation method can provide the engineers a more efficient way to design and optimize a servo valve and an overall servo system.     

Stochastic sensitivity analysis of coupled acoustic-structural systems under non-stationary random excitations

This paper presents a new sensitivity analysis method for coupled acoustic–structural systems subjected to non-stationary random excitations. The integral of the response power spectrum density (PSD) of the coupled system is taken as the objective function. The thickness of each structural element is used as a design variable. A time-domain algorithm integrating the pseudo excitation method (PEM), direct differentiation method (DDM) and high precision direct (HPD) integration method is proposed for the sensitivity analysis of the objective function with respect to design variables. Firstly, the PEM is adopted to transform the sensitivity analysis under non-stationary random excitations into the sensitivity analysis under pseudo transient excitations. Then, the sensitivity analysis equation of the coupled system under pseudo transient excitations is derived based on the DDM. Moreover, the HPD integration method is used to efficiently solve the sensitivity analysis equation under pseudo transient excitations in a reduced-order modal space. Numerical examples are presented to demonstrate the validity of the proposed method.     

基于遗传算法的舰载IMU优化布局

惯性测量单元（IMU）用来为舰载武器系统提供准确的姿态并实时监测舰船甲板的变形，对其数目和位置进行优化具有重要的实用价值．提出了多IMU优化布局的原则，建立了舰载IMU优化布局的数学模型，采用遗传算法对IMU的布局进行了优化求解。仿真结果表明，舰载IMU的布局是影响甲板变形估计精度的一个重要因素，通过对IMU的布局进行优化，减少了舰载武器系统所需IMU的数量；利用优化布局后IMU的输出信息对全舰甲板变形进行估计，估计精度有很大提高。     

Optimum design of a supercavitating torpedo considering overall size,shape, and structural configuration

A supercavitating torpedo is a complex high speed undersea weapon that is exposed to extreme operating conditions due to the weapon’s speed. To successfully design a torpedo that can survive in this environment, it is necessary to consider the torpedo shell as a critical component. The shell of a supercavitating torpedo must be designed to survive extreme loading conditions (depth pressure and thrust loading), meet frequency constraints, and fit inside the cavity generated by the cavitator. In this research, an algorithm to determine the optimal configuration of the torpedo is presented. This method formulates an optimization problem that determines the general shape of the torpedo in order to satisfy the required performance criteria. Simultaneously, a method to determine the optimal stiffener configuration in the torpedo structure is also presented. A torpedo configuration for a desired speed is obtained and the details of the process are thoroughly discussed.     

Synchronization of stochastic reaction–diffusion systems via boundary control

This paper studies the problem of mean square asymptotical synchronization and \(H_\infty \) synchronization for coupled stochastic reaction–diffusion systems (SRDSs) via boundary control. Based on the deduced synchronization error dynamic, we design boundary controllers to achieve mean square asymptotical synchronization. By virtue of Lyapunov functional method and Wirtinger’s inequality, sufficient conditions are obtained for ensuring mean square asymptotical synchronization. When coupled SRDSs are subject to external disturbance, mean square \(H_\infty \) synchronization is investigated and corresponding criterion is presented under a designed boundary controller. In addition to focusing on systems with Neumann boundary conditions, we also briefly study coupled SRDSs with mixed boundary conditions and sufficient conditions are provided to achieve the desired performance. Numerical examples are used to verify the effectiveness of our theoretical results.     

Approximate solving method of shock for nonlinear disturbed coupled Schrödinger system

A class of nonlinear disturbed coupled Schrödinger systems is studied. The specific technique is used to relate the exact and approximate solutions. The corresponding typical coupled system is considered. An exact shock travelling solution is obtained by a mapping method. The travelling asymptotic solutions of the disturbed coupled Schrödinger system are then found with an approximate method.