临近空间高超声速目标拦截弹弹道规划

利用弹道规划设计了针对临近空间高超声速飞行器的拦截弹道。分析了临近空间高超声速目标拦截问题,将其定性为临近空间的远程高超声速拦截,并提出弹道规划需求;设计了一种两级助推的拦截弹,建立了考虑地球曲率和自转的拦截弹质点平面运动模型;根据弹道规划需求设计弹道约束,以末速最大、与终点距离误差最小和全程热量最小为指标建立拦截弹弹道规划问题;采用粒子群算法求解弹道,结果表明:符合约束的规划弹道是高抛再入形式,与比例导引弹道和准最佳弹道相比,拦截弹大部分时间飞行在大气层外,有效降低了气动热效应影响和对弹体材料的性能需求,且为末制导段提供良好的初始工作环境。     

US strategic preferences in the early twenty-first century

This article investigates how US national security planners have envisioned the emerging strategic environment during the early twenty-first century and evaluates how their perceptions of this strategic environment have changed during these years. This conceptual evolution can be seen in how defense planners define threats, identify defense priorities, and design security strategies. Five key strategic planning documents serve as the basis for this analysis and illustrate significant shifts in how the US government has envisioned its own security requirements as well as the context within which its strategic vision will need to be realized. These planning documents are: (1) Joint Vision 2020, (2) the Bush Administration's 2002 National Security Strategy of the United States, (3) the Obama Administration's 2010 National Security Strategy, (4) US Strategic Defense Guidance entitled Sustaining US Global Leadership: Priorities for 21^st Century Defense, and (5) the US Chairman of the Joint Chiefs of Staff's Capstone Concept for Joint Operations: Joint Force 2020.     

平流层飞艇高能激光武器防御弹道导弹

防御弹道导弹逐渐受到世界各国的重视,扩大拦截窗口是重要的发展趋势之一。平流层飞艇有可能通过艇载激光武器或者中继反射地基激光两种方式拦截自由段弹道导弹,为评估这两种方式的拦截效果和可行性,本文分析了平流层飞艇搭载高能激光武器的可能性以及中继反射作战方式的特点,建立了激光烧蚀模型,采用数值计算方法对激光的烧蚀效果进行了研究,结果表明平流层飞艇部署位置应距离导弹发射点800～1000km,平流层中继激光飞艇能够在短时间内引爆弹头,艇载激光武器采用烧蚀弹头防热层的方法同样可以达到拦截弹道导弹的目的。     

基于路径规划的虚拟人上肢可触及性检查技术

针对目前虚拟人上肢可触及性检查操作烦琐、效率低的问题,提出一种RRT（Rapidly-exploring RandomTree）算法与逆向运动学算法相结合的路径规划方法,通过检测可行路径是否存在来实现人体上肢可触及性检查。给出了该方法的具体流程和关键问题的解决策略,并基于Jack软件进行了实例验证。     

驱护舰编队对海作战中舰载无人机任务规划

任务规划是舰载无人机作战使用的基础。根据舰载无人机作战性能特点,从作战使用的角度对舰载无人机任务规划的概念进行了诠释,提出将舰载无人机的任务规划区分为战术规划和航迹规划,给出了舰载无人机任务规划应遵循的原则以及任务规划的内容和步骤,提出了舰载无人机在驱护舰编队对海作战中可遂行的战术任务。     

反向设计方法在防空导弹中的应用研究

对反向设计方法在防空导弹中的应用进行初步探讨。重点讨论了导弹总体、气动以及动力系统之间的关系。针对国外典型防空导弹,建立了反向设计模型,结合弹道仿真研究了国外典型防空导弹的战技指标、关键技术以及发展趋势。     

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.     

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。