高超声速伸缩翼变形飞行器轨迹多目标优化

针对高超声速条件下变形技术的应用模式，对具有伸缩翼的组合式飞行器滑翔弹道进行了多目标优化研究。介绍了伸缩翼的变形模式，给出了不同变形状态下的气动特性；建立了三自由度滑翔轨迹动力学模型和伸缩翼前缘热流计算模型；采用MOEA/D多目标优化算法，以变形条件和飞行攻角为设计变量、以最大射程和最小翼前缘总吸热量为目标函数，进行了多目标优化计算。优化结果表明，MOEA/D计算得到了相对均匀分布的Pareto最优解集，将伸缩翼外形与无变形外形相比，飞行器滑翔段射程得到了显著提高，同时伸缩翼前缘总吸热量有明显的降低。     

基于复杂网络的作战网络分析

分布式网络化作战是网络中心战的基础,而分布式作战网络的构建是网络化作战的重要前提。首先,运用复杂网络的相关参数分析了多种不同的网络,选择了BA非标度网络作为分布式作战网络的最优表现形式;其次,以BA非标度网络为基础提出了一个适合军事上动态鲁棒性分析的模型DCNCE;最后,仿真结果表明,在以网络效能值为测度的对比下,分布式作战网络在介数毁伤策略下更脆弱,为构建并改进现有的作战网络提供了理论依据。     

Benders' cuts guided large neighborhood search for the traveling umpire problem

This article introduces the use of Benders' cuts to guide a large neighborhood search to solve the traveling umpire problem, a sports scheduling problem inspired by the real‐life needs of the officials of a sports league. At each time slot, a greedy matching heuristic is used to construct a schedule. When an infeasibility is recognized first a single step backtracking is tried to resolve the infeasibility. If unsuccessful, Benders' cuts are generated to guide a large neighborhood search to ensure feasibility and to improve the solution. Realizing the inherent symmetry present in the problem, a large family of cuts are generated and their effectiveness is tested. The resulting approach is able to find better solutions to many instances of this problem. © 2011 Wiley Periodicals, Inc. Naval Research Logistics, 2011     

Polynomial‐time approximation scheme for concurrent open shop scheduling with a fixed number of machines to minimize the total weighted completion time

In this article, we consider the concurrent open shop scheduling problem to minimize the total weighted completion time. When the number of machines is arbitrary, the problem has been shown to be inapproximable within a factor of 4/3 ‐ ε for any ε > 0 if the unique games conjecture is true in the literature. We propose a polynomial time approximation scheme for the problem under the restriction that the number of machines is fixed. © 2011 Wiley Periodicals, Inc. Naval Research Logistics, 2011     

Batch scheduling on a two‐machine jobshop with machine‐dependent setup times

The problem of minimum makespan on an m machine jobshop with unit execution time (UET) jobs (m ≥ 3) is known to be strongly NP‐hard even with no setup times. We focus in this article on the two‐machine case. We assume UET jobs and consider batching with batch availability and machine‐dependent setup times. We introduce an efficient \begin{align*}(O(\sqrt{n}))\end{align*} algorithm, where n is the number of jobs. We then introduce a heuristic for the multimachine case and demonstrate its efficiency for two interesting instances. © 2011 Wiley Periodicals, Inc. Naval Research Logistics, 2011     

A genetic algorithm with neighborhood search for the resource‐constrained project scheduling problem

The resource‐constrained project scheduling problem (RCPSP) consists of a set of non‐preemptive activities that follow precedence relationship and consume resources. Under the limited amount of the resources, the objective of RCPSP is to find a schedule of the activities to minimize the project makespan. This article presents a new genetic algorithm (GA) by incorporating a local search strategy in GA operators. The local search strategy improves the efficiency of searching the solution space while keeping the randomness of the GA approach. Extensive numerical experiments show that the proposed GA with neighborhood search works well regarding solution quality and computational time compared with existing algorithms in the RCPSP literature, especially for the instances with a large number of activities. © 2011 Wiley Periodicals, Inc. Naval Research Logistics, 2011     

基于RBF神经网络的直接自适应飞行控制器

设计了一种径向基神经网络(RBF NN)飞行控制器结构,并给出了相应的控制律和参数调节律。由于调节了RBF NN的全部参数(连接权、高斯函数的中心和宽度),得到了很好的控制性能。以F8战斗机为控制对象进行了仿真分析,仿真表明,在存在70%的模型误差的情况下,该控制器仍然能实现较好的跟踪控制,表现出很好的鲁棒性,远远优于传统的只调节连接权值的算法。     

面向对象方法的一类飞行器模拟器设计与实现

对一类C4I飞行器模拟器的设计与实现进行了研究.该模拟器是分布式C4I仿真系统中的兵力生成子系统,起着演示指控效果、检验决策质量的重要作用.从系统需求出发,采用面向对象的方法对它进行了分析与设计,并最终实现了飞行器模拟器软件系统.该系统已成功应用于某防空C4I仿真试验床中,C4I联机试验表明,飞行器模拟器能较好地模拟指控命令响应并提供较高精度的飞行导航模拟数据.此外,面向对象方法的采用,不仅使系统功能得到了加强,也大大缩短了系统的开发周期.     

小型无人机航位推算定位算法研究与误差分析

对空中航位推算(DR)算法做了深入研究,提出了适用于小型无人机(UAV)的风速估计策略;将算法中各元素的误差对推算定位精度的影响进行了理论分析与数值计算;该研究结果应用于某小型UAV的航位推算/GPS组合导航系统的设计与实现中;飞行试验表明,通过提高对DR误差影响较大的元素的测量精度和风速的估计精度,有效提高了DR推算精度,与以往其他小型UAVs相比,在断开GPS对DR的修正后,DR精度保持在一定范围的持续时间显著延长.     

甲板坐标系下速率火控射击诸元解算及弹道修正

速率火控系统是在甲板坐标系下解相遇的,它不依赖于导航系统.它与常规火控不同,甲板倾斜的修正不能采用简单的坐标系变换的方式.针对速率火控甲板倾斜修正问题,指出了两种需要进行甲板倾斜修正的情况,推导给出了计算方法,通过原理仿真计算,验证了计算方法的正确性.