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George Kozanidis 《先进运输杂志》2009,43(2):155-182
Every aircraft, military or civilian, must be grounded for maintenance after it has completed a certain number of flight hours since its last maintenance check. In this paper, we address the problem of deciding which available aircraft should fly and for how long, and which grounded aircraft should perform maintenance operations, in a group of aircraft that comprise a combat unit. The objective is to achieve maximum availability of the unit over the planning horizon. We develop a multiobjective optimization model for this problem, and we illustrate its application and solution on a real life instance drawn from the Hellenic Air Force. We also propose two heuristic approaches for solving large scale instances of the problem. We conclude with a discussion that gives insight into the behavior of the model and of the heuristics, based on the analysis of the results obtained. 相似文献
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随着中国民航事业的快速发展,航班不正常变得越来越严重.虽然航空运输系统涉及空管、航空公司与机场三方面,但是目前解决不正常航班却单纯依靠空管.而这种方式无法达到减少不正常航班的目的.本文研究在协同决策机制下,航空公司自由指派航班时隙的方法问题.文中建立航班时隙指派模型,针对模型的特点设计了一种参数启发式算法。最后通过实例证明了采用本文的方法可以减少航班总延误时间并且提高航班正点率.通过该实例说明航空公司参与时隙分配决策的重要性. 相似文献
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Gábor Orosz 《Vehicle System Dynamics: International Journal of Vehicle Mechanics and Mobility》2016,54(8):1147-1176
Connected vehicle systems (CVS) are considered in this paper where vehicles exchange information using wireless vehicle-to-vehicle (V2V) communication. The concept of connected cruise control (CCC) is established that allows control design at the level of individual vehicles while exploiting V2V connectivity. Due to its high level of modularity the proposed design can be applied to large heterogeneous traffic systems. The dynamics of a simple CVS is analysed in detail while taking into account nonlinearities in the vehicle dynamics as well as in the controller. Time delays that arise due to intermittencies and packet drops in the communication channels are also incorporated. The results are summarised using stability charts which allow one to select control gains to maintain stability and ensure disturbance attenuation when the delay is below a critical value. 相似文献
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编队飞行是实现民航绿色发展的重要措施之一。在前机尾涡危险区域分析的基础上,科学确定后机最优位置是编队飞行的关键。首先,以随机两阶段尾涡消散模型为基础,利用Hallock-Burnham涡模型和诱导滚转力矩系数模型分析后机诱导滚转力矩系数的演变规律。然后,基于设定的安全阈值,给出前机尾涡危险区域,并考虑飞行高度、速度和风对危险区域的影响。最后,基于后机不同位置处的燃油流量减少率,得出编队飞行中后机最优位置。研究结果表明:后机诱导滚转力矩系数随着前、后机之间横向距离的增加,呈先增后减再增的趋势;随纵向距离的增加,呈先缓慢减小后快速减小的趋势;高度越高、速度越小,诱导滚转力矩系数的峰值越高。飞行高度越高、速度越小,前机初始尾涡的危险区域越大;随着纵向距离的增加,危险区域不断减小,并随涡核的下沉不断下降。侧风使危险区域发生偏离,侧风越大,偏离程度越大。顺风会增加危险区域的纵向距离,顶风则与之相反。两架B737-800飞机在12000 m高度以0.78马赫数进行编队飞行时,前、后机纵向距离3000m处,无风情况下后机最优位置为横向距离30 m
或-30 m、垂直距离29 m,此时燃油流量减少率为7.01%。相较于无风,左侧风20 m·s
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下,燃油流量减少率和垂直距离不变,横向距离增加;顺风20 m·s
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下,燃油流量减少率增加,横向距离不变,垂直距离减少;顶风20 m·s
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下,燃油流量减少率减小,横向距离不变,垂直距离增加。 相似文献
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为提高交通流运行的机动性、稳定性,对车辆协同巡航控制(CACC)系统进行了改进设计. 基于经典Newell 模型提出了考虑CACC的改进跟驰模型,分析了所提出的CACC改进跟驰模型的动力学特性,给出了CACC改进跟驰模型的线性稳定性条件,并对由CACC车辆和非CACC车辆组成的非均匀车队的不同无线通讯拓扑结构进行了比较研究. 通过数值试验进一步研究了在起步、刹车和意外事件的情况下,CACC车辆的存在对交通流动力学的影响. 研究结果表明,通过合理设计CACC跟驰系统的模型参数取值后,CACC车辆的存在一方面可以提高交通流运行的机动性与稳定性,另一方面可以使交通出行更加的安全和舒适. 此外,由于不同车队中CACC车辆的无线通讯拓扑结构会影响交通流的机动性与稳定性,对于 CACC车辆的无线通讯拓扑结构应慎重的设计与优化. 相似文献