多边形障碍环境中避障路径的遗传算法

研究了平面障碍环境中避障的遗传算法,重点介绍了障碍环境的模型构造和用遗传算法求解该模型的方法设计.采用了与已有遗传算法不同的染色体编码方式和不同的遗传算子设计,在初始群体产生时尽量避免了引入无效基因,提高了染色体进化的效率,使得该算法具有很好的寻优能力,实验结果也表明了该算法的有效性.     

势场理论的多无人机协同路径规划方法

在势场理论的基础上对穿越多威胁区的无人机路径进行了协同规划,在规划中将每个威胁区按实际情况分为极危险区域和次危险区域,而这些威胁不仅包括己方情报所得的已知威胁,而且包括在执行攻击任务过程中新发现的突发威胁,然后利用物理学中的扩散方程建立势场,并在已建立的势场中对多无人机进行整体协同路径规划。在建立模型的同时,进行了仿真模拟,仿真结果表明了该方法的正确性和可行性。     

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     

Failure profiles of coherent systems

In this paper we first introduce and study the notion of failure profiles which is based on the concepts of paths and cuts in system reliability. The relationship of failure profiles to two notions of component importance is highlighted, and an expression for the density function of the lifetime of a coherent system, with independent and not necessarily identical component lifetimes, is derived. We then demonstrate the way that failure profiles can be used to establish likelihood ratio orderings of lifetimes of two systems. Finally we use failure profiles to obtain bounds, in the likelihood ratio sense, on the lifetimes of coherent systems with independent and not necessarily identical component lifetimes. The bounds are relatively easy to compute and use. © 2004 Wiley Periodicals, Inc. Naval Research Logistics, 2004     

基于SWOT分析的军队审计容错免责机制完善路径研究

军队审计容错免责机制是在审计权限范围内对符合容错免责情形的事由减轻或免于问责并及时纠正的稳定工作机制,是审计问责态势下应对“为官不为”问题的合理路径。本文基于SWOT法分析认为,当前审计环境下建立军队审计容错免责机制的优势在于独立的经济监督地位、专业的经济监督力量和广泛的经济监督对象,劣势在于单一的认定主体、缺失的法律规范和匮乏的免责素质,机遇在于利好政策的出台、国家审计的实践经验和军队审计的职能定位,威胁在于制度规范笼统、审计风险扩大和资源矛盾加剧。在此基础上,本研究基于W-T（劣势-威胁）的战略选择,提出完善军队审计容错免责机制的现实路径,即：明确机制定位,科学界定边界;完善制度规范,形成法律依据;完备容错清单,转变审计模式;优化容错环境,降低容错风险。     

具有节点失效的网络可靠度的信息交互算法

提出了一种用于计算具有节点失效的网络可靠度的新计算方法。该算法依据不交化代数及协同计算的思想,采用节点信息义互的方法直接获得网络的不交化最小路集。算法简便易行,具有分布计算的特点,为大型网络系统的可靠性度计算提供了一种新的途径。     

Optimal motion planning in rapid‐fire combat situations with attacker uncertainty

This article provides a modeling framework for quantifying cost and optimizing motion plans in combat situations with rapid weapon fire, multiple agents, and attacker uncertainty characterized by uncertain parameters. Recent developments in numerical optimal control enable the efficient computation of numerical solutions for optimization problems with multiple agents, nonlinear dynamics, and a broad class of objectives. This facilitates the application of more realistic, equipment‐based combat models, which track both more realistic models, which track both agent motion and dynamic equipment capabilities. We present such a framework, along with a described algorithm for finding numerical solutions, and a numerical example.     

基于威胁路径的报警关联分析方法

大量的误报大大降低了现有网络入侵检测系统的实用性,利用报警日志之间的逻辑关系是降低误报率的方法之一。提出了威胁路径的概念,在此基础上提出了基于因果关系的关联分析方法。利用网络的背景信息,发掘报警日志记录之间的逻辑关系,进一步提高报警的准确性,降低误报率。经实验验证,该方法可有效降低网络入侵检测系统误报率,并可用于辅助分析网络入侵过程。     

翼伞系统线目标归航方法

针对运载火箭助推器或子级无控坠落地面落点散布较大的情况,提出一种翼伞系统的线目标归航方法。建立了矩形边界下的归航计算模型,对点目标归航和线目标归航两种方法进行了收缩区域分析;对翼伞归航能力、落区散布边界特征对归航性能的影响进行对比分析,得到了相应的归航策略,并提出在较大散布区域下设置多个着陆区域的工程解决方案;建立动力学和操纵控制模型,对线目标归航过程进行了仿真。结果表明,所提方法对工程有一定的参考价值。     

基于路径跟踪的平流层飞艇柔性编队控制

建立平流层飞艇驻空阶段动力学模型,在定高飞行前提下,采用小扰动方法对动力学方程进行线性化处理。提出采用路径跟踪的平流层飞艇柔性领航-跟随编队控制方法,领航者和跟随者通过速度控制与航向控制,分别跟踪保持特定距离的参考路径,实现编队的柔性控制。以采用直线路径跟踪和采用圆路径跟踪的三平流层飞艇编队控制为例,对提出的柔性编队控制方法进行仿真验证。仿真结果表明:提出的路径跟踪方法控制精度高,提出的柔性编队控制方法可以实现编队稳定运行,避免编队成员碰撞现象的发生。