基于熵值法的坦克动力舱热工况的综合评价

坦克动力舱的结构和布置有多种型式,为了对不同结构的动力舱热工况的优劣进行对比、评价,必须用量化的指标加以衡量.提出了一种坦克动力舱热工况的评价指标体系,运用熵值法原理科学地确定各评价指标权重,建立了综合评价模型,并对某型主战坦克动力舱的不同布置方案进行了热工况综合评价.     

维恩位移定律2种表述之间的关系

讨论了维恩位移定律2种表述之间的关系,并与麦克斯韦分子分布函数的峰值相关量进行对比,说明原始的维恩表述是由实验决定的.并对2种表述的物理意义作了阐述.     

自动变速车辆换挡规律的研究

研究了自动变速车辆的换挡规律的算法,制定了车辆的动力性换挡规律和经济性换挡规律,建立了车辆动力学仿真模型.通过仿真,分析了不同换挡规律对车辆性能的影响.     

模糊合成算子在作战方案综合评估的应用研究

在分布式交互仿真中,根据仿真结果对作战方案进行综合评估,运用模糊综合评判的方法进行评判,并着重对合成算子的选择进行分析,确定乘与有界算子M(·, )为比较适合对作战方案评估的算子.     

Appointment scheduling at a multidisciplinary outpatient clinic using stochastic programming

The purpose of this paper is to investigate the problem of constructing an appointment template for scheduling patients at a specific type of multidisciplinary outpatient clinic called an integrated practice unit (IPU). The focus is on developing and solving a stochastic optimization model for a back pain IPU in the face of random arrivals, an uncertain patient mix, and variable service times. The deterministic version of the problem is modeled as a mixed integer program with the objective of minimizing a weighted combination of clinic closing time (duration) and total patient waiting time (length of stay). A two‐stage stochastic program is then derived to account for the randomness and the sequential nature of the decisions. Although it was not possible to solve the two‐stage problem for even a limited number of scenarios, the wait‐and‐see (WS) problem was sufficiently tractable to provide a lower bound on the stochastic solution. The introduction of valid inequalities, limiting indices, and the use of special ordered sets helped to speed up the computations. A greedy heuristic was also developed to obtain solutions much more quickly. Out of practical considerations, it was necessary to develop appointment templates with time slots at fixed intervals, which are not available from the WS solution. The first to be derived was the expected value (EV) template that is used to find the expected value of the EV solution (EEV). This solution provides an upper bound on the objective function value of the two‐stage stochastic program. The average gap between the EEV and WS solutions was 18%. Results from extensive computational testing are presented for the EV template and for our adaptation of three other templates found in the literature. Depending on the relative importance of the two objective function metrics, the results demonstrate the trade‐off that exists between them. For the templates investigated, the “closing time” ranged from an average of 235 to 275 minutes for a 300‐minute session, while the corresponding “total patient time in clinic” ranged from 80 to 71 minutes.     

高空气球地面充氦气量计算方法分析与试验评估

作为高空气球研究中的一个重要问题,气球在地面发放前充入的氦气量会直接影响其上升速度和驻空高度,进而影响平台的可靠性和稳定性。因此研究充氦气量的准确计算方法十分必要。建立了高空气球上升过程动力学模型,计算了气球初始升速的理论值,用于与实际初始升速对比,为评估充氦气量计算方法提供依据。归纳了三种较为典型的高空气球地面充氦气量计算方法,根据实际开展的飞行试验,分析对比了三种方法的准确性和误差范围。提出了浮力补偿规律,完成了对三种方法的评估。通过研究可以对现有充氦气量计算方法进行有效修正,进而为高空气球的实际飞行提供指导。     

军事刑事诉讼概念研究

军事刑事诉讼既是国家刑事诉讼的有机组成部分,同时又是与普通刑事诉讼相对而言的一种特殊刑事诉讼。对国家刑事诉讼来说,二者是部分与整体的关系;对普通刑事诉讼来说,二者则是个别与一般的关系。军事刑事诉讼之所以有存在的必要,不是基于它的一般性,而是基于它的特殊性。军事刑事诉讼的特殊性主要体现在刑事诉讼主体、刑事诉讼内容、刑事诉讼程序等三个方面。     

空间拦截末制导段能量需求分析

为了研究空间拦截末制导段的能量需求,对导航与测轨误差模式和空间拦截交会条件进行了分析,并建立末制导段仿真模型。使用Monte-Carlo法仿真,获得不同交会角下和不同拦截概率下拦截器所需的能量,并讨论了交会角和相对速度对拦截器能量需求的影响。     

基于变系数的变前置角导引律设计

对基于变系数的变前置角导引律进行了分析与研究,并从理论上给出了该导引规律的推导过程,然后对整个弹道系统建立仿真模型,并对理论设计的导引方法进行数学仿真计算。将所得到的仿真结果与经典的前置角法进行比较分析,得出最终结论。从而验证该方法的有效性。     

一体化装备保障指挥体系的内涵及结构模型

在分析、界定一体化装备保障指挥体系相关概念的基础上,建立了一体化装备保障指挥体系结构模型,并且围绕未来信息化条件下联合作战装备保障的需求,探讨了构建一体化装备保障指挥体系亟待解决的问题及对策.