某杀伤弹与某子母弹弹道一致性设计

为进行某杀伤弹与某子母弹弹道一致性设计,通过FLUENT对弹丸外流场进行数值仿真,获取相关的气动力参数.用仿真结果进行阻力特性分析和射程估算,根据分析结果进行设计方案调整并进行试验验证,结果表明调整方案满足设计要求,说明采用数值仿真方法设计弹丸气动外形是有效、可行的.     

高架桥声屏障高度对高速列车气动特性的影响

针对现代高速铁路建设中大量采用高架桥的现况,为保证列车安全、舒适、环保运行,给高速铁路建设工程提供参考数据,研究行驶在高架桥上的高速列车气动特性.利用FLUENT模拟单线高架桥声屏障高度对高速列车气动特性的影响.将声屏障分为6种不同高度,不考虑横向风且列车运行速度为200 km/h.地面和高架桥均设为移动壁面边界条件,...     

基于改进型精密整流电路的电容式微位移传感器设计

介绍了一种改进型精密整流电路,该电路基于一个模拟多路复用器,无需二极管和匹配电阻,克服了传统整流电路中的非线性问题。同时基于该精密整流电路设计了一种电容式微位移传感器。测试结果表明,在0～1.6mm的量程内,该电容式微位移传感器的非线性误差小于0.6‰,灵敏度约为4.3V/mm。     

悬臂梁大变形的向量式有限元分析

为分析悬臂梁的几何非线性行为,用向量式有限元法将结构离散成质点系以及质点间的连接单元.根据牛顿第二定律得到每个质点在内力和外载荷作用下的运动方程以及悬臂梁在每个时刻的变形用该时刻质点系的运动表示.结合刚架元的节点内力和等效质量得出质点位移的迭代计算公式,采用FORTRAN编制计算程序,对悬臂梁分别承受集中载荷和弯矩下的大变形进行算例分析.计算结果与理论解吻合较好,表明该方法能很好地模拟分析悬臂梁的大变形.     

面向分级设计优化的飞行器参数化建模方法

针对飞行器气动隐身外形综合设计优化问题,提出合适的面向分级设计优化流程,建立适应该流程的渐进分层参数化建模方法;用基于敏度分析的参数影响程度分析方法筛选复杂设计变量;采用多学科设计优化（Multidisplinary Design Optimization,MDO）理论和差分进化算法进行飞行器气动隐身外形的综合设计优化.将该方法用于某飞行器外形设计优化,结果表明：该方法合理可行,可为飞行器外形多学科设计优化提供一定参考.     

基于SVM与遗传算法的非线性模式识别

设计了一种支持向量机的模型结构,以遗传算法进行该模型参数的组合优化建模,并将其用于非线性模式识别,该方法不仅对线性问题有效,对非线性问题同样适用有效;该法简洁易行,优于多段线性分类器设计方法与BP误差回传网络算法,通过实例验证其识别效率达100％。     

星载气象雷达功放非线性对超低副瓣脉冲压缩信号的影响及消除

为在强海面回波影响下测量反射较弱的雨云.星载气象雷达要求脉冲压缩的主副瓣功率比高于60 dB.因此超低副瓣脉冲压缩成为星载气象雷达的核心技术之一.超低副瓣的实现对线性度要求很高.星载雷达为保证发射机的功率和效率,功放多工作于近饱和区,造成副瓣电平恶化.本文分析了功放非线性对超低副瓣脉冲压缩信号的影响,基于射频功率放大器、矢量信号发生仪和矢量信号分析仪实现了功放数字预失真算法,并利用松弛迭代法提高了迭代收敛速度.在保证星载气象雷达超低副瓣的前提下提高了发射机的功效.     

考虑非线性项的卫星编队保持

针对低轨道运行的编队卫星在非线性项作用下,伴随卫星运行的相对运动轨道发生偏移的情况,传统的李亚普诺夫方法能较好地控制轨道的初始偏移,使系统达到李亚普诺夫大范围一致稳定,但长期项误差震荡较大.本文提出了一种多回路结构的卫星轨道保持的控制方法,内回路选取使系统满足李亚普诺夫大范围一致稳定的控制律,外回路选取LQR线性状态调节器.此内外回路调节器能更好地抑制环绕卫星相对于基准轨道的误差漂移,更好地稳定编队队形.最后,数值仿真结果验证了此方法比传统的李亚普诺夫方法具有使编队更稳定的效果.     

Finite element formulation for dynamics of planar flexible multi-beam system

In some previous geometric nonlinear finite element formulations, due to the use of axial displacement, the contribution of all the elements lying between the reference node of zero axial displacement and the element to the foreshortening effect should be taken into account. In this paper, a finite element formulation is proposed based on geometric nonlinear elastic theory and finite element technique. The coupling deformation terms of an arbitrary point only relate to the nodal coordinates of the element at which the point is located. Based on Hamilton principle, dynamic equations of elastic beams undergoing large overall motions are derived. To investigate the effect of coupling deformation terms on system dynamic characters and reduce the dynamic equations, a complete dynamic model and three reduced models of hub-beam are prospected. When the Cartesian deformation coordinates are adopted, the results indicate that the terms related to the coupling deformation in the inertia forces of dynamic equations have small effect on system dynamic behavior and may be neglected, whereas the terms related to coupling deformation in the elastic forces are important for system dynamic behavior and should be considered in dynamic equation. Numerical examples of the rotating beam and flexible beam system are carried out to demonstrate the accuracy and validity of this dynamic model. Furthermore, it is shown that a small number of finite elements are needed to obtain a stable solution using the present coupling finite element formulation.     

Geometric nonlinear effects on the planar dynamics of a pivoted flexible beam encountering a point-surface impact

Flexible-body modeling with geometric nonlinearities remains a hot topic of research by applications in multibody system dynamics undergoing large overall motions. However, the geometric nonlinear effects on the impact dynamics of flexible multibody systems have attracted significantly less attention. In this paper, a point-surface impact problem between a rigid ball and a pivoted flexible beam is investigated. The Hertzian contact law is used to describe the impact process, and the dynamic equations are formulated in the floating frame of reference using the assumed mode method. The two important geometric nonlinear effects of the flexible beam are taken into account, i.e., the longitudinal foreshortening effect due to the transverse deformation, and the stress stiffness effect due to the axial force. The simulation results show that good consistency can be obtained with the nonlinear finite element program ABAQUS/Explicit if proper geometric nonlinearities are included in the floating frame formulation. Specifically, only the foreshortening effect should be considered in a pure transverse impact for efficiency, while the stress stiffness effect should be further considered in an oblique case with much more computational effort. It also implies that the geometric nonlinear effects should be considered properly in the impact dynamic analysis of more general flexible multibody systems.