某型滑翔增程靶弹方案弹道设计

针对某滑翔增程靶弹的无动力特性,综合各方面因素,提出一种具有近似平飞段的方案弹道。选择相关参数,设计了一种具有近似平飞段的高度变化律,提出了改进的攻角表达式,得到无动力靶弹三自由度铅垂平面的运动模型。数字仿真证明,这种方法合理可行,满足了靶弹各项战技指标,实现靶弹的近似平飞,方案弹道能较好地追踪给定高度变化,具有较高的工程应用价值。     

一种无人地面车的轨迹跟踪控制方法

针对无人地面车辆经典轨迹跟踪控制方法的不足,提出了一种基于无人地面车辆运动学模型的轨迹跟踪控制算法。在算法中引入了位姿的纵坐标误差,以加快跟踪的逼近速度,并利用人工驾驶的思想,采用了一种位一姿交替控制的方法,使路径跟踪既准确又快速。仿真结果表明：该方法是有效的,且可使无人地面车具有更好的跟踪性能。     

增程修正弹单炮多发同时弹着火控技术研究

针对大口径火炮使用增程修正弹打远修近问题,建立了增程修正弹单炮多发同时弹着的控制算法,仿真验证了算法可在不同射程上实现单炮多发同时弹着,对发挥舰炮作战效能具有一定的意义。     

助推-滑翔飞行器弹道分段优化研究

通过数值计算得到了升力体飞行器的气动参数,利用Radau伪谱法将助推-滑翔飞行器弹道优化问题转化为非线性规划问题,分别对主动段和滑翔段进行优化,通过仿真得到了飞行器从助推到滑翔的完整弹道,分析了主动段性能指标对飞行器最大射程的影响。研究结果表明,采用主动段关机点速度最大为性能指标的优化方案,其射程最大,且实现难度适中。     

Random disambiguation paths for traversing a mapped hazard field

We consider the problem of safely and swiftly navigating through a spatial arrangement of potential hazard detections in which each detection has associated with it a probability that the detection is indeed a true hazard. When in close proximity to a detection, we assume the ability—for a cost—to determine whether or not the hazard is real. Our approach to this problem involves a new object, the random disambiguation path (RDP), which is a curve‐valued random variable parametrized by a binary tree with particular properties. We prove an admissibility result showing that there is positive probability that the use of an RDP reduces the expected traversal length compared to the conventional shortest zero‐risk path, and we introduce a practically computable additive‐constant approximation to the optimal RDP. The theoretical considerations are complemented by simulation and example. © 2005 Wiley Periodicals, Inc. Naval Research Logistics, 2005     

Economic ordering decisions with market choice flexibility

Standard approaches to classical inventory control problems treat satisfying a predefined demand level as a constraint. In many practical contexts, however, total demand is comprised of separate demands from different markets or customers. It is not always clear that constraining a producer to satisfy all markets is an optimal approach. Since the inventory‐related cost of an item depends on total demand volume, no clear method exists for determining a market's profitability a priori, based simply on per unit revenue and cost. Moreover, capacity constraints often limit a producer's ability to meet all demands. This paper presents models to address economic ordering decisions when a producer can choose whether to satisfy multiple markets. These models result in a set of nonlinear binary integer programming problems that, in the uncapacitated case, lend themselves to efficient solution due to their special structure. The capacitated versions can be cast as nonlinear knapsack problems, for which we propose a heuristic solution approach that is asymptotically optimal in the number of markets. The models generalize the classical EOQ and EPQ problems and lead to interesting optimization problems with intuitively appealing solution properties and interesting implications for inventory and pricing management. © 2003 Wiley Periodicals, Inc. Naval Research Logistics, 2004.     

基于改进核极限学习机和集成学习理论的目标机动轨迹预测

为了提高目标轨迹预测的精度以及预测模型的泛化能力,提出基于改进蝙蝠算法优化的核极限学习机(Kernel Extreme Learning Machine,KELM)和集成学习理论目标机动轨迹预测模型。构建KELM模型,并采用改进的蝙蝠算法对KELM的参数进行优化;以优化后的KELM神经网络为弱预测器,结合集成学习算法生成强预测器,通过训练不断优化强预测的结构和参数,得到一种基于集成学习理论的目标机动轨迹预测模型;基于不同规模的样本,将所得预测模型与逆传播神经网络、支持向量机和极限学习机等模型进行对比分析。仿真结果表明:所提目标机动轨迹预测模型具有较好的预测精度和泛化能力。     

多UCAV协同作战自主任务规划系统

在分析未来多UCAV协同作战任务的基础上,构建了一个多UCAV协同作战的自主任务规划系统结构,探讨了其运行机制。提出这个系统的核心是自主规划器,它应该具有任务分解、智能信息处理和机载任务规划与重规划能力。设计了自主规划器的初步方案。指出了这个系统下一步研究的任务和方向。     

基于Simulink的质点外弹道模型仿真

介绍了基于Simulink的质点外道模型的设计与仿真方法。首先给出了地面直角坐标系下的弹丸质心运动方程组,然后介绍如何采用Simulink建立系统的仿真模型并进行仿真计算。仿真方法具有模型设计过程简单、修改容易和结果直观等特点,可以应用到刚体弹道、火箭弹道及控制弹道等模型的仿真。     

助推-滑翔式导弹中段弹道方案的初步分析

建立了助推—滑翔式弹道中段的无量纲运动方程。采用非线性规划方法实现弹道优化。首先求解不同初始速度、速度倾角和最大升阻比的最大射程弹道,然后考虑驻点热流、过载约束,求解总气动加热最小和射程最大的最优弹道。基于前者的计算结果分析了初始条件对最大射程弹道的影响。将考虑约束的再入滑翔弹道与弹道式再入的特征参数比较,表明再入滑翔弹道的峰值热流较小,而总气动加热增加,但再入滑翔飞行时间在一般锥形体再入机动飞行器的热防护系统可承受的时间范围内。