弹体压心位置变化对末制导炮弹弹道的影响

首先对比弹体压心位置变化对火箭增程弹道和末制导炮弹名义弹道的不同影响，重点分析弹体压心位置变化对末制导炮弹末导段弹道的影响特点，得出弹体压心位置变化对末导段弹道的捕获域和有效攻击区有着重要影响的结论。该结论对末制导炮弹的射表编拟以及新型末制导炮弹的设计都具有重要指导意义。     

公共场所人员安全疏散评价方法探讨

公共场所安全疏散评价对于确保火灾中人员的生命安全具有重要意义。基于“性能化”防火设计的思想，对影响公共场所安全疏散的因素进行了分析，并对安全疏散的必要性能和评价程序进行了较为全面的探讨，其中包括烟气的评价、人员疏散能力的评价、疏散路线合理性的评价、疏散对策的评价等，目的在于通过合理的评价方法得出合理的疏散性能，为减少公共场所火灾造成的人员伤亡和财产损失提供帮助。     

An attacker‐defender model for analyzing the vulnerability of initial attack in wildfire suppression

Wildfire managers use initial attack (IA) to control wildfires before they grow large and become difficult to suppress. Although the majority of wildfire incidents are contained by IA, the small percentage of fires that escape IA causes most of the damage. Therefore, planning a successful IA is very important. In this article, we study the vulnerability of IA in wildfire suppression using an attacker‐defender Stackelberg model. The attacker's objective is to coordinate the simultaneous ignition of fires at various points in a landscape to maximize the number of fires that cannot be contained by IA. The defender's objective is to optimally dispatch suppression resources from multiple fire stations located across the landscape to minimize the number of wildfires not contained by IA. We use a decomposition algorithm to solve the model and apply the model on a test case landscape. We also investigate the impact of delay in the response, the fire growth rate, the amount of suppression resources, and the locations of fire stations on the success of IA.     

飞机反区速度矢量不稳定及其控制的机理

在信号流图的基础上,提出多回路分析的方法,并用于研究反区时速度矢量不稳定及其稳定控制的机理。建立了纵向动力学的信号流图,并证明了一个回路的收敛性定理。在此基础上,通过理论分析得出了速度矢量不稳定在不同层面上的原因,也得出了速度和轨迹的发散度表达式等,并表明阻力-速度曲线、轨迹角-速度曲线、极曲线、阻力系数曲线等存在相互对应的反区和正区,并且阻力-速度曲线和轨迹角-速度曲线在斜率上成比例。研究得出进场动力补偿系统下速度矢量的稳定临界条件、收敛度、稳定机理等,理论分析和仿真比较了速度恒定进场动力补偿系统和迎角恒定进场动力补偿系统在控制性能上的差异。     

抛物线用作雷达阵地地面有效反射区曲线

讨论了传统的米波雷达地面有效反射区和粗糙地面的选择条件,提出采用抛物线作为地面反射区曲线,并给出曲线公式,各反射点的反射波在主要方向同相叠加增加了探测距离,进一步挖掘了米波雷达的威力潜力;合理选择反射区曲线的长度,可减少近地物反射的杂波,提高低空目标的探测能力。     

无先验信息排除无源交叉定位虚假交点的新方法

提出了一种排除无源交叉定位虚假交点的新方法,称为四边形分组法.该方法通过将无源交叉定位产生的四边形进行分组来区分真实交点和虚假交点.这种方法只需要测向信息,不需要任何其他先验信息.该方法无需先验信息.仿真结果表明,该方法是有效的,运算速度快,对水平编队目标群定位精度高.     

电视制导无人攻击机可攻击域研究

分析了电视制导无人攻击机的制导原理,建立了该电视制导无人攻击机空间六自由度运动方程组,给出了电视制导无人攻击机控制系统数学模型和控制信号的形成模型。在气动力参数的处理上,用最小二乘法拟合技术建立了电视制导无人攻击机的气动力参数模型,保证了参数理论求解的精度。最后对电视制导无人攻击机的可攻击域进行仿真计算,分析了影响可攻击域的因素,验证了电视制导无人攻击机的攻击能力。     

Dynamic server assignment policies for assembly‐type queues with flexible servers

We seek dynamic server assignment policies in finite‐capacity queueing systems with flexible and collaborative servers, which involve an assembly and/or a disassembly operation. The objective is to maximize the steady‐state throughput. We completely characterize the optimal policy for a Markovian system with two servers, two feeder stations, and instantaneous assembly and disassembly operations. This optimal policy allocates one server per station unless one of the stations is blocked, in which case both servers work at the unblocked station. For Markovian systems with three stations and instantaneous assembly and/or disassembly operations, we consider similar policies that move a server away from his/her “primary” station only when that station is blocked or starving. We determine the optimal assignment of each server whose primary station is blocked or starving in systems with three stations and zero buffers, by formulating the problem as a Markov decision process. Using this optimal assignment, we develop heuristic policies for systems with three or more stations and positive buffers, and show by means of a numerical study that these policies provide near‐optimal throughput. Furthermore, our numerical study shows that these policies developed for assembly‐type systems also work well in tandem systems. © 2008 Wiley Periodicals, Inc. Naval Research Logistics, 2008     

隧道火灾机械通风临界风速研究

由于隧道的半封闭性,空间有限,当长度很长时空气流通不畅,一旦发生火灾,烟气就会迅速填充隧道,而且CO等危险气体也会随烟气向隧道扩散,这对隧道内车辆和人员造成极大的危险。因此,需要保证隧道内空气流通状态的良好以及发生火灾时对烟气的良好控制。模拟了隧道口附近发生一定功率火灾的情况下,控制烟气层流动所需要的临界风速。     

满足大动压模拟要求的试验弹道优化设计

为了解决弹道导弹在高海拔发射场进行飞行试验时的大动压检验问题,提出一种模拟大动压条件的试验弹道设计方法。针对发射场的实际特点,建立残骸再入的动力学模型与落区边界模型;将大动压模拟条件转化为过程约束,提出一种主动段联合优化策略。基于自适应模拟退火算法,分别设计了三组满足不同大动压模拟条件和各项约束的试验弹道,并给出了对应的落区调整方案,验证了该方法的可行性。设计结果表明,最大动压主要出现在一级,一级最大负攻角增加,则最大动压也明显提高;同时调整发射方位角和二、三级程序角可以保证试验弹道满足弹头落点约束条件。