纯方位目标运动分析四维状态的最小二乘模型及分析

建立了纯方位系统TMA四维状态的最小二乘模型,详细给出了非线性最小二乘算法的迭代公式,分析了非线性最小二乘模型、线性最小二乘模型可解的必要条件,以及非线性最小二乘模型与极大似然模型的等价性。     

Dynamic evacuation routes for personnel on a naval ship

We propose a dynamic escape route system for emergency evacuation of a naval ship. The system employs signals that adapt to the causative contingency and the crew's physical distribution about the ship. A mixed‐integer nonlinear programming model, with underlying network structure, optimizes the evacuation process. The network's nodes represent compartments, closures (e.g., doors and hatches) and intersections, while arcs represent various types of passageways. The objective function integrates two potentially conflicting factors: average evacuation time and the watertight and airtight integrity of the ship after evacuation. A heuristic solves the model approximately using a sequence of mixed‐integer linear approximating problems. Using data for a Spanish frigate, with standard static routes specified by the ship's designers, computational tests show that the dynamic system can reduce average evacuation times, nearly 23%, and can improve a combined measure of ship integrity by up to 50%. In addition, plausible design changes to the frigate yield further, substantial improvements. Published 2008 Wiley Periodicals, Inc. Naval Research Logistics 2008     

运载器牵制释放结构动力响应数值模拟方法研究

将运载器牵制释放垂直发射的过程依次分为静态、牵制、释放三个阶段.利用MSC.Patran/Nastran的场功能和分组分析功能,将前一个阶段的计算结果场向后一个阶段的初始条件场传递,提出了一种分析运载器牵制释放全过程结构动力响应的分阶段计算新方法.解决了牵制释放过程中由于出现运载器-发射台分离面给结构动力响应计算带来的困难.采用该方法计算了几个运载器牵制释放的算例,分析了牵制阶段牵制力的变化、释放阶段运载器结构动力响应的特点、不同释放时间对结构动力响应的影响.算例表明:该方法实施简便、精度较高,还可拓展用于不同时刻释放、释放不同步、施加缓释力等条件下运载器结构动力响应的分析,为牵制释放系统的研制提供参考.     

坦克炮控伺服系统的滑模非线性摩擦补偿控制

坦克炮控伺服系统存在低速摩擦,摩擦环节不但造成系统的稳态误差,而且导致极限环振荡、低速爬行等现象.提出基于Lyapunov稳定理论的滑模控制方法,通过 Lyapunov稳定理论获得控制量,同时克服参数不确定性和补偿非线性摩擦力矩,从而保证跟踪误差渐进收敛.仿真结果表明该设计方法大大优于经典设计,为炮控伺服系统实际设计提供了一种可行的新方法.     

一类具Holling-Ⅲ类功能性反应的食物有限捕食-被捕食模型的极限环

研究一类具Holling-Ⅲ类功能性反应的食物有限捕食-被捕食模型的动力学性态。应用微分方程定性理论,证明当正平衡点不稳定时该模型存在唯一稳定的极限环。     

SS-IUKF算法及其在成像声纳组合导航中的应用

利用成像声纳对海底进行探测时需要高精度的导航信息。针对导航高维滤波问题,文中在球面单形sigma点变换的基础上,将其与迭代UKF相结合,提出了球面单形迭代无迹卡尔曼滤波(SS-IUKF)算法,并应用于捷联惯性导航系统(SINS)/多普勒流速剖面仪(ADCP)组合导航系统。仿真结果表明,SS-IUKF算法相比UKF、SR-UKF、EKF算法提高了滤波精度和计算速度,具有一定的工程应用价值。     

第19届国际信息融合会议及获奖论文评述

总结了第19届国际信息融合会议的总体情况和主要特点,通过对大会报告、分会场报告以及国际信息融合界一些著名专家团队发表论文情况的统计分析,提炼出国际信息融合界普遍关注的焦点和难点问题;通过对获奖论文的分析,了解到受大会评奖委员会一致认可的年度优秀成果和技术进步点;最后,面向高层信息融合中的不确定性处理,对信息融合领域的发展进行展望。     

频域加权LQR控制器改进设计

基于线性二次型调节器(Linear Quadratic Regulator,LQR)控制方法,设计一种频域加权LQR控制器;通过对其常用滤波器进行改进,提出一种新型滤波器设计思路.当振源频率低于执行器下限响应频率,导致执行器输出减小时,通过改变滤波器参数、增大低频部分权重及控制力,可提高低于执行器响应下限频段的控制性能...     

用弹性动力学基本分析方法求解导弹 折叠翼展开的动响应

用机构弹性动力学的基本方法分析了一种导弹折叠翼展开的动力学问题,详细介绍了运动微分方程的解法,并将计算结果曲线与刚体动力学计算曲线、试验测得的曲线进行比较和分析,证明了该算法的可靠性和可行性。     

Response surface analysis of two‐stage stochastic linear programming with recourse

We apply the techniques of response surface methodology (RSM) to approximate the objective function of a two‐stage stochastic linear program with recourse. In particular, the objective function is estimated, in the region of optimality, by a quadratic function of the first‐stage decision variables. The resulting response surface can provide valuable modeling insight, such as directions of minimum and maximum sensitivity to changes in the first‐stage variables. Latin hypercube (LH) sampling is applied to reduce the variance of the recourse function point estimates that are used to construct the response surface. Empirical results show the value of the LH method by comparing it with strategies based on independent random numbers, common random numbers, and the Schruben‐Margolin assignment rule. In addition, variance reduction with LH sampling can be guaranteed for an important class of two‐stage problems which includes the classical capacity expansion model. © 1999 John Wiley & Sons, Inc. Naval Research Logistics 46: 753–776, 1999