高旋弹头滑块控制的建模与仿真

建立了双滑块机构下的高旋弹头动力学分析模型,对气动力矩变化和惯量张量变化给外弹道参数带来的影响进行了仿真研究,结果表明:双滑块机构对弹道三维方向的改变均有效果,同时弹头飞行攻角也是逐渐减小,因此系统的稳定性也是可以得到保证的,这就为后续的闭环控制提供了必要的保证.     

复杂约束下的导弹作战任务规划模型和算法研究*

导弹作战任务规划是一个涉及时间、资源、质量和其他关系约束的复杂问题.首先通过定叉约束满足效用对基本约束满足模型进行了扩展,建立了导弹任务规划的约束满足优化模型.在此基础上,研究了任务规划模型求解的时间和效用传播算法,提出了基于综合效用的优化求解框架.该模型和求解框架易于解决具有多种约束因素的复杂问题,具有较好的通用性.通过定义软、硬约束效用,使得实际任务规划问题求解具有更好的灵活性.     

Disaster management in case of CBRNe events: an innovative methodology to improve the safety knowledge of advisors and first responders

Nowadays, Chemical-Biological-Radiological-Nuclear-explosive (CBRNe) risks are one of the world's main safety concerns. The radiological disasters of Fukushima and Chernobyl, the chemical events of Seveso or the release of Sarin in the Tokyo Subway, the biological emergencies such as the H1N1 flu or the recent Ebola outbreak, and recent news about the availability of non-conventional weapons acquired by fundamentalist organisations represent evidence of potential future threats. CBRNe risks are a real and global threat. The University of Rome, Tor Vergata, in collaboration with the most important Italian and international bodies working in the field of CBRNe safety and security, and supported by the North Atlantic Treaty Organisation and the Organisation for the Prohibition of Chemical Weapons, organises International Masters Courses on the Protection against CBRNe events. Within this framework, a Table-Top Exercise was planned, in collaboration with the Italian Ministry of Interior and Ministry of Defence. The scenario, the logistic organisation, on-going adjustments during the exercise and the outcomes are presented here and analysed.     

舰炮弹道估计的卡尔曼滤波算法

针对舰炮弹道观测校正中的弹道最佳估计问题,提出了转换卡尔曼滤波算法,在三维空间里对观测弹丸飞行轨迹进行滤波,估计最佳弹道。给出了具体的算法并用某型海军舰炮进行了仿真,取得了较好效果。     

Column generation for stochastic green telecommunication network planning with switchable base stations

We present the green telecommunication network planning problem with switchable base stations, where the location and configuration of the base stations are optimized, while taking into account uncertainty and variability of demand. The problem is formulated as a two‐stage stochastic program under demand uncertainty with integers in both stages. Since solving the presented problem is computationally challenging, we develop the corresponding Dantzig‐Wolfe reformulation and propose a solution approach based on column generation. Comprehensive computational results are provided for instances of varying characteristics. The results show that the joint location and dynamic switching of base stations leads to significant savings in terms of energy cost. Up to 30% reduction in power consumption cost is achieved while still serving all users. In certain cases, allowing dynamic configurations leads to more installed base stations and higher user coverage, while having lower total energy consumption. The Dantzig‐Wolfe reformulation provides solutions with a tight LP‐gap eliminating the need for a full branch‐and‐price scheme. Furthermore, the proposed column generation solution approach is computationally efficient and outperforms CPLEX on the majority of the tested instances. © 2016 Wiley Periodicals, Inc. Naval Research Logistics 63: 351–366, 2016     

火箭-双燃烧室冲压组合循环发动机概念研究

临近空间高超声速飞行器近年来获得了广泛关注,本文提出一种以基于火箭发动机和双燃烧室冲压发动机的多模态火箭-双燃烧室冲压组合循环发动机作为飞行器的动力系统,并进行了性能分析研究。该飞行器在海拔10 km左右高度以0.8马赫的速度投放,在重力和发动机推力的联合作用下,能够在海拔5～8 km处加速到2马赫;然后加速爬升进入临近空间,发动机工作在引射亚燃或者双燃烧室亚燃模态下。可以根据实际选择高推重比、较低推进剂比冲效率的引射亚燃模态,或是较低推重比、高推进剂比冲效率的双燃烧室亚燃模态。最终飞行器加速到6马赫(26 km),进入双燃室超燃模态。针对空中发射模式和地面发射模式进行了轨道优化,仿真结果表明:在加速爬升到6马赫(26 km)的过程中,空中发射模式相比较地面发射模式可以节省37%的推进剂;空中发射模式存在一个负的最优初始飞行角度使得剩余质量与初始质量的比值达到最大。     

末修迫弹修正效果影响因素分析

在对脉冲控制迫弹末修原理简单介绍的基础上，在六自由度弹道模型上进行了蒙特卡洛仿真打靶试验。分析在落点预测导引模式和XZ追踪导引模式下，脉冲启控时刻、脉冲个数和修正模式对修正效果的影响，并对两种导引模式修正原理和特点进行详细的对比分析，得到两种导引模式下确定脉冲参数的原则。     

指令制导防空炮弹启控点参数的确定方法

简要阐述了指令制导防空炮弹有控弹道控制模式,建立了鸭舵控制力和控制力矩作用下的有控弹道模型,研究了弹丸理想启控姿态和启控位置的确定方法,得到了确定理想启控位置的启控函数.数值仿真结果表明,该启控函数简单、快速,具有较高精度,易于计算机程序实现,弹丸有控弹道也可保持飞行稳定.研究结果对今后深入展开指令制导防空炮弹的研究和工程设计具有一定的参考意义.     

飞行器航路规划算法分析

针对现代军用飞行器任务规划系统航路规划的特点,分析了飞行器航路规划的基本要求,阐述了目前国内外应用和研究的几种航路规划算法:A*搜索算法、遗传算法、粒子群算法、数学规划算法、电势理论法等,并对飞行器航路规划算法的发展趋势进行了展望.     

A bidirectional heuristic for maximizing the net present value of large‐scale projects subject to limited resources

We consider the scheduling of large‐scale projects to maximize the project net present value given temporal and resource constraints. The net present value objective emphasizes the financial aspects of project management. Temporal constraints between the start times of activities make it possible to handle practical problem assumptions. Scarce resources are an expression of rising cost. Since optimization techniques are not expedient to solve such problems and most heuristic methods known from literature cannot deal with general temporal constraints, we propose a new bidirectional priority‐rule based method. Scheduling activities with positive cash flows as early and activities with negative cash flows as late as possible results in a method which is completed by unscheduling techniques to cope with scarce resources. In a computational experiment, we compare the well‐known serial generation scheme where all activities are scheduled as early as possible with the proposed bidirectional approach. On the basis of a comprehensive data set known from literature containing instances with up to 1002 activities, the efficiency of the new approach is demonstrated. © 2003 Wiley Periodicals, Inc. Naval Research Logistics, 2003