基于遗传算法反舰导弹航路规划研究

航路规划作为提高反舰导弹作战能力的重要措施,目前正逐渐被反舰导弹所应用。结合反舰导弹自控飞行特点,系统分析航路规划过程中各个航路点的约束条件,并运用遗传算法进行数学建模和计算机编程,顺利实施了导弹航路的最优求解和航路的自动标绘,为指挥员实施导弹攻击提供辅助决策。     

Optimal capacity in a coordinated supply chain

We consider a supply chain in which a retailer faces a stochastic demand, incurs backorder and inventory holding costs and uses a periodic review system to place orders from a manufacturer. The manufacturer must fill the entire order. The manufacturer incurs costs of overtime and undertime if the order deviates from the planned production capacity. We determine the optimal capacity for the manufacturer in case there is no coordination with the retailer as well as in case there is full coordination with the retailer. When there is no coordination the optimal capacity for the manufacturer is found by solving a newsvendor problem. When there is coordination, we present a dynamic programming formulation and establish that the optimal ordering policy for the retailer is characterized by two parameters. The optimal coordinated capacity for the manufacturer can then be obtained by solving a nonlinear programming problem. We present an efficient exact algorithm and a heuristic algorithm for computing the manufacturer's capacity. We discuss the impact of coordination on the supply chain cost as well as on the manufacturer's capacity. We also identify the situations in which coordination is most beneficial. © 2008 Wiley Periodicals, Inc. Naval Research Logistics, 2008     

Optimal timing of switches between product sales for sports and entertainment tickets

Like airlines and hotels, sports teams and entertainment venues can benefit from revenue management efforts for their ticket sales. Teams and entertainment venues usually offer bundles of tickets early in their selling horizon and put single‐event tickets on sale at a later date; these organizations must determine the best time to offer individual tickets because both types of ticket sales consume the same fixed inventory. We model the optimal a priori timing decision for a seller with a fixed number of identical tickets to switch from selling the tickets as fixed bundles to individual tickets to maximize the revenue realized before the start of the performance season. We assume that bundle and single‐ticket customers each arrive according to independent, nonhomogeneous Markovian death processes with a linear death rate that can vary over time and that the benefit from selling a ticket in a package is higher than from selling the ticket individually. We characterize the circumstances in which it is optimal for the seller to practice mixed bundling and when the seller should only sell bundles or individual tickets, and we establish comparative statics for the optimal timing decision for the special case of constant customer arrival rates. We extend our analytical results to find the optimal time for offering two groups of tickets with high and low demand. Finally, we apply the timing model to a data set obtained from the sports industry. © 2007 Wiley Periodicals, Inc. Naval Research Logistics, 2008     

ATIE:一种自适应的可调域间出口选择算法

TIE算法能对域间出口的选择进行调节,但是该算法的参数计算过于复杂,并且出口选择的调节并不能随负载的变化而变化,因此提出了一种自适应的可调域间出口选择算法ATIE,该算法能够满足流量工程和网络健壮性要求,并通过参数T的改变随当前负载的变化而变化.实验表明,ATIE算法能够在控制剖面敏感性和随负载变化的流量工程自适应性上达到合理的折衷.     

基于运载能力评估的固体运载火箭推力向量控制方案比较

从对运载能力影响角度开展固体运载火箭发动机推力向量控制系统比较分析研究。设计了三种采用不同发动机推力向量控制系统的多级固体运载火箭方案,将增广乘子法与共轭方向法相结合,对固体运载火箭上升段弹道进行了优化设计,给出运载能力评估结果。研究表明,起飞质量均为50 000kg,目标轨道均为300km太阳同步轨道时,采用栅格舵和侧喷流作为推力向量控制系统方案,比采用燃气舵和侧喷流作为推力向量控制系统方案,运载能力提高70kg,比各级固体发动机全部采用摆动喷管控制方案,运载能力提高115kg,为固体运载火箭总体方案论证提供理论依据。     

雷达组网系统责任区抗干扰优化部署

针对有源压制干扰对雷达组网系统的威胁,深入分析了雷达组网系统的抗干扰优化部署问题,建立了雷达组网系统责任区抗干扰优化布站决策模型,并给出了具体的算法和求解分析.仿真结果验证了该方法的有效性,可为雷达组网系统的实际优化部署提供参考.     

空地多目标序贯攻击三维最优航迹实现

单机或多机协同执行对地多目标攻击任务将成为未来空地战争的一种重要形式。制定了合适的分段规划策略,建立了水平面和垂直面的空地多目标序贯攻击最优航迹模型,应用经典的可行方向法对模型求解。根据水平面和垂直面规划的相互关系及规划结果,得到三维最优航迹,为飞行导航提供有效依据。最后通过实例验证了所建模型及方法的有效性。     

高超声速飞行器俯冲机动最优制导方法

为解决高超声速飞行器俯冲段精确制导与机动突防问题,研究了机动突防最优制导方法。针对零化视线角速率降低突防性能的问题,在俯冲平面及转弯平面内分别设计了正弦形式的视线角参考运动,同时为进一步实现俯冲精确制导,以落速最大为性能指标利用最优控制对其进行跟踪,引入了伪控制量以简化最优制导问题的求解,最后分析了该方法的稳定性及制导性能。以CAV-H为例进行仿真分析,仿真结果表明该方法能够实现机动飞行,且能够高精度地满足终端落角及落点约束,可为高超声速飞行器俯冲段精确制导及机动突防提供参考。     

基于频率优化组合的KBR系统时标误差校正

时标误差是K波段精密测距仪(KBR)的一个重要测距误差源,现有的时标误差校正方法依赖于对星间时标偏差的精确测量。针对目前我国星间时标偏差测量精度不能满足校正需求的问题,提出了基于双频优化组合的时标误差校正方法,推导了优化频率之间应该满足的定量关系。研究了双频优化组合的实现,指出原有的KBR系统无法实现频率优化,在此基础上设计实现了一种改进频率流程的KBR系统,并对新的时标误差校正方法进行了实验验证。实验结果表明,基于双频优化组合的时标误差校正方法和改进的KBR系统有效降低了对星间时标偏差测量精度的要求。     

基于二阶锥规划的MIMO雷达任意形状旁瓣波束设计

针对MIMO雷达非均匀布阵引起的高旁瓣问题,提出一种基于二阶锥规划的任意形状旁瓣设计算法.算法通过在旁瓣区域附加多个二次不等式约束,从而有效抑制干扰、保持期望方向天线增益的同时,获得了期望的、可以任意控制的旁瓣波束响应.通过将优化模型转化为凸二阶锥规划问题,利用内点法可以得到有效求解.仿真试验表明:算法能够获得任意形状期望旁瓣波束设计的同时,有效提高了波束形成器的输出信干燥比.最后计算机仿真结果证实了算法的有效性和可行性.