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101.
A bicriterion approach to common flow allowances due window assignment and scheduling with controllable processing times 下载免费PDF全文
We investigate a single‐machine scheduling problem for which both the job processing times and due windows are decision variables to be determined by the decision maker. The job processing times are controllable as a linear or convex function of the amount of a common continuously divisible resource allocated to the jobs, where the resource allocated to the jobs can be used in discrete or continuous quantities. We use the common flow allowances due window assignment method to assign due windows to the jobs. We consider two performance criteria: (i) the total weighted number of early and tardy jobs plus the weighted due window assignment cost, and (ii) the resource consumption cost. For each resource consumption function, the objective is to minimize the first criterion, while keeping the value of the second criterion no greater than a given limit. We analyze the computational complexity, devise pseudo‐polynomial dynamic programming solution algorithms, and provide fully polynomial‐time approximation schemes and an enhanced volume algorithm to find high‐quality solutions quickly for the considered problems. We conduct extensive numerical studies to assess the performance of the algorithms. The computational results show that the proposed algorithms are very efficient in finding optimal or near‐optimal solutions. © 2017 Wiley Periodicals, Inc. Naval Research Logistics, 64: 41–63, 2017 相似文献
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可控翼伞系统在飞行器回收领域有广阔的应用前景。本文就可控翼伞系统建立了六自由度数学模型,并用该模型对40m~2可控翼伞系统的滑翔和稳定性进行了仿真计算和分析,研究结果对可控翼伞系统设计和实验有一定参考价值。 相似文献
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本文采用修正的周期图法(Welch法)对舰船磁场信号进行了功率谱估计并给出归一化曲线。在此基础上,提取了频域特征量,利用特征频率f_H进行了目标舰船速度的识别研究。计算机仿真表明,正识率可达95%以上。 相似文献
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用药室增长量预估线膛火炮初速下降量精度很低,根据火炮身管烧蚀磨损特点,本文提出了用身管严重磨损段阳线磨损量表征火炮初速减退量,在130mm加农炮上所做试验表明,用该方法可提高大口径火炮初速下降量的预估精度。 相似文献
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本文研究了弹体旋转角速度测量的机理,采用极化栅网,使弹体的反射信号包含有弹体的旋转角速度信息,并且通过实验予以证明。文中提出了一种旋转角速度测量系统。本文对测量弹体旋转角速度是有一定帮助的。 相似文献
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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。 相似文献
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The prediction of the fragment velocity distribution of a cylindrical cased charge with end caps is one of the key issues to assess the damage efficiency of the warhead. However, limited work has been con-ducted to predict the fragment velocity distributions along the axis of cylindrical cased charges with end caps. This paper presents a study of the velocity distribution of fragments caused by the explosion of a cylindrical cased charge with end caps. The fragment velocity distribution and the end cap velocity were determined by an X-ray radiography method, and the axial fragment distribution was determined by witness plates. It was found that the velocities of fragments, especially near the edge, were increased when the end caps were added, and the position of maximum velocity is closer to the non-detonation end. The fragment velocities were increased, and the fragment projection range was decreased with the increase of the thickness of the end cap. A formula for fragment velocity distributions of a cylindrical cased charge with end caps, which is based on Huang's formula, was proposed by the theoretical analysis and data fitting and validated experimentally. The results indicate that the proposed formula is accurate in predicting the fragment velocity distribution along the axis of a cylindrical cased charge with end caps detonated at one end. 相似文献