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舰艇编队航渡中多机伴随反潜研究 被引量:1
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作者 罗木生 王俊敏 梁春芳 《电光与控制》 北大核心 2014年第12期20-24,29,共6页
针对舰艇编队航渡过程中的多架舰载反潜直升机前出执行伴随反潜作战问题进行研究。通过分析潜射鱼雷射距,建立了理想条件与编队规避机动两种情况下的鱼雷攻击阵位模型,从而得出伴随反潜区的阵位配置。在此基础上,对编队航渡过程中的多... 针对舰艇编队航渡过程中的多架舰载反潜直升机前出执行伴随反潜作战问题进行研究。通过分析潜射鱼雷射距,建立了理想条件与编队规避机动两种情况下的鱼雷攻击阵位模型,从而得出伴随反潜区的阵位配置。在此基础上,对编队航渡过程中的多机伴随反潜方法进行了分析,并建立了伴随反潜兵力需求与探测概率模型。最后仿真计算了潜射鱼雷发射阵位,以及反潜兵力数量、探测次数、伴随反潜区大小对发现概率的影响。结果表明,伴随反潜区配置在编队前方20 n mile处,大小为20 n mile×30 n mile,反潜直升机数量3架为宜。 展开更多
关键词 伴随反潜 舰艇编队 反潜阵位配置 航渡过程 动规避 鱼雷攻击
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空中加油最优分配方案设计 被引量:3
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作者 王功明 王秀琴 +1 位作者 吴华瑞 赵春江 《计算机工程与设计》 CSCD 北大核心 2007年第10期2422-2425,共4页
设计空中加油最优分配方案具有极其重要的应用价值。按加油位置不同,加油机分伴随机和接应机两种,确定两种辅机分配个数、加油点和加油量是问题求解关键。首先利用独立性原理,求出单独使用伴随机和接应机时局部最优方案,然后利用计算机... 设计空中加油最优分配方案具有极其重要的应用价值。按加油位置不同,加油机分伴随机和接应机两种,确定两种辅机分配个数、加油点和加油量是问题求解关键。首先利用独立性原理,求出单独使用伴随机和接应机时局部最优方案,然后利用计算机组合搜索全局最优方案,使问题得到圆满解答。本模型通用性强,既可用计算机求解,也可查表求解,有一定理论参考和实际应用价值。 展开更多
关键词 空中加油 作战半径 伴随机 接应 独立性 飞行增益 组合
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Two-stage vs single-stage management for concomitant gallstones and common bile duct stones 被引量:108
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作者 Jiong Lu Yao Cheng +3 位作者 Xian-Ze Xiong Yi-Xin Lin Si-Jia Wu Nan-Sheng Cheng 《World Journal of Gastroenterology》 SCIE CAS CSCD 2012年第24期3156-3166,共11页
AIM:To evaluate the safety and effectiveness of twostage vs single-stage management for concomitant gallstones and common bile duct stones.METHODS:Four databases,including PubMed,Embase,the Cochrane Central Register o... AIM:To evaluate the safety and effectiveness of twostage vs single-stage management for concomitant gallstones and common bile duct stones.METHODS:Four databases,including PubMed,Embase,the Cochrane Central Register of Controlled Trials and the Science Citation Index up to September 2011,were searched to identify all randomized controlled trials(RCTs).Data were extracted from the studies by two independent reviewers.The primary outcomes were stone clearance from the common bile duct,postoperative morbidity and mortality.The secondary outcomes were conversion to other procedures,number of procedures per patient,length of hospital stay,total operative time,hospitalization charges,patient acceptance and quality of life scores.RESULTS:Seven eligible RCTs [five trials(n = 621) comparing preoperative endoscopic retrograde cholangiopancreatography(ERCP)/endoscopic sphincterotomy(EST) + laparoscopic cholecystectomy(LC) with LC + laparoscopic common bile duct exploration(LCBDE);two trials(n = 166) comparing postoperative ERCP/EST + LC with LC + LCBDE],composed of 787 patients in total,were included in the final analysis.The metaanalysis detected no statistically significant difference between the two groups in stone clearance from the common bile duct [risk ratios(RR) =-0.10,95% confidence intervals(CI):-0.24 to 0.04,P = 0.17],postoperative morbidity(RR = 0.79,95% CI:0.58 to 1.10,P = 0.16),mortality(RR = 2.19,95% CI:0.33 to 14.67,P = 0.42),conversion to other procedures(RR = 1.21,95% CI:0.54 to 2.70,P = 0.39),length of hospital stay(MD = 0.99,95% CI:-1.59 to 3.57,P = 0.45),total operative time(MD = 12.14,95% CI:-1.83 to 26.10,P = 0.09).Two-stage(LC + ERCP/EST) management clearly required more procedures per patient than single-stage(LC + LCBDE) management.CONCLUSION:Single-stage management is equivalent to two-stage management but requires fewer procedures.However,patient's condition,operator's expertise and local resources should be taken into account in making treatment decisions. 展开更多
关键词 Laparoscopic cholecystectomy Laparoscop-ic common bile duct exploration Endoscopic retrogradecholangiopancreatography Endoscopic sphincterotomy GALLSTONES Common bile duct stones META-ANALYSIS
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一种针对组网雷达的突防行动任务规划策略
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作者 张清博 李云龙 +2 位作者 张博 吴长宇 李伟 《火力与指挥控制》 CSCD 北大核心 2021年第12期73-80,共8页
组网雷达探测系统是构成预警监视、防空警戒、目标引导、导弹防御等军事防御体系的关键环节。信息化条件下的空中作战行动对敌方组网雷达实施电子干扰是获取“制磁权”、夺取信息优势,并为后续空中火力打击开辟通道的主要手段。针对多... 组网雷达探测系统是构成预警监视、防空警戒、目标引导、导弹防御等军事防御体系的关键环节。信息化条件下的空中作战行动对敌方组网雷达实施电子干扰是获取“制磁权”、夺取信息优势,并为后续空中火力打击开辟通道的主要手段。针对多机伴随式协同干扰组网雷达关键技术展开研究,对远距离支援干扰机进行分析,确定其干扰目标、干扰策略及巡航路径;建立多机伴随式协同干扰模型,寻求突防机群的最佳航迹,实现在远距离支援干扰机和随队支援干扰机掩护下安全抵达攻击线;最终确定在不同时刻的干扰策略和干扰功率分配,完成针对组网雷达的突防行动任务规划。这一工作对飞行部队完成突防任务具有一定的参考价值。 展开更多
关键词 远距离支援干扰 伴随式协同干扰 雷达对抗 干扰策略
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Concomitant chemoradiation using gemcitabine in locally advanced hepatocellular carcinoma
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作者 Abdul Mateen Abrar Ahmed Javed Ahmed Ijaz Masood 《The Chinese-German Journal of Clinical Oncology》 CAS 2012年第3期130-133,共4页
Objective:Hepatocellular carcinoma (HCC) is among the most common and rapidly increasing cancers in Pakistan.There is currently no standard management for advanced HCC.The aim of the study was to assess response rate ... Objective:Hepatocellular carcinoma (HCC) is among the most common and rapidly increasing cancers in Pakistan.There is currently no standard management for advanced HCC.The aim of the study was to assess response rate and toxicity of concomitant gemcitabine and external radiation therapy (ERT) in locally advanced HCC.Methods:Sixty patients were enrolled.Gemcitabine,70 mg/m2 was given weekly during ERT.ERT was delivered with 60Co beam up to 30.6 Gy,1.8 Gy/fraction.Tumor response was assessed by computed tomography (CT) at eight weeks.Complete and partial response (CR and PR),progressive and stable disease (PD and SD) were assessed.Hematological,gastrointestinal and hepatic toxicities were assessed weekly.Results:No CR was seen.PR,SD and PD were seen in 33%,40% and 27% of patients respectively.Grade 3/4 toxicity for total leukocyte count and platelets was observed in 7% and 27% patients.Grade 3/4 toxicity for liver failure,bilirubin,aspartate aminotransferase,alanine aminotransferase and alkaline phosphatase was seen in 35%,28%,38%,24% and 43% patients respectively.Conclusion:The study showed that concomitant gemcitabine and ERT is a feasible option with moderate toxicity in advanced HCC. 展开更多
关键词 chemotherapy GEMCITABINE hepatocellular carcinoma (HCC) RADIOTHERAPY
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空中加油最优分配建模与实现
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作者 王功明 王秀琴 +1 位作者 郭新宇 赵春江 《数学的实践与认识》 CSCD 北大核心 2010年第5期79-86,共8页
确定最佳空中加油方案,既有一定难度,又有重要的实用价值.本文针对加油机可以多次上天情况,对这一问题展开研究,确定了使主机飞行距离最大的空中加油方案.我们将飞机飞行过程分为出航和返航两个阶段,首先利用数学归纳法得出出航阶段的... 确定最佳空中加油方案,既有一定难度,又有重要的实用价值.本文针对加油机可以多次上天情况,对这一问题展开研究,确定了使主机飞行距离最大的空中加油方案.我们将飞机飞行过程分为出航和返航两个阶段,首先利用数学归纳法得出出航阶段的最佳加油方案;然后对返航过程建立约束方程组,求出返航阶段的最佳加油方案.利用这一模型结果可以对任意多架加油机的情况确定全程最佳加油方案.最后结合出航、返航编队及飞行姿态调整对模型作了一定范围的定量扩展,使本文的研究更具有实用价值. 展开更多
关键词 空中加油 作战半径 伴随机 接应 飞行增益
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Study on Adjoint-Based Optimization Method For Multi-Stage Turbomachinery 被引量:6
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作者 Weiwei Li Yong Tian +3 位作者 Weilin Yi Lucheng Ji Weiwei Shao Yunhan Xiao 《Journal of Thermal Science》 SCIE EI CAS CSCD 2011年第5期398-405,共8页
Adjoint-based optimization method is a hotspot in turbomachinery.First,this paper presents principles of adjoint method from Lagrange multiplier viewpoint.Second,combining a continuous route with thin layer RANS equat... Adjoint-based optimization method is a hotspot in turbomachinery.First,this paper presents principles of adjoint method from Lagrange multiplier viewpoint.Second,combining a continuous route with thin layer RANS equations,we formulate adjoint equations and anti-physical boundary conditions.Due to the multi-stage environment in turbomachinery,an adjoint interrow mixing method is introduced.Numerical techniques of solving flow equations and adjoint equations are almost the same,and once they are converged respectively,the gradients of an objective function to design variables can be calculated using complex method efficiently.Third,integrating a shape perturbation parameterization and a simple steepest descent method,a frame of adjoint-based aerodynamic shape optimization for multi-stage turbomachinery is constructed.At last,an inverse design of an annular cascade is employed to validate the above approach,and adjoint field of an Aachen 1.5 stage turbine demonstrates the conservation and areflexia of the adjoint interrow mixing method.Then a direct redesign of a 1+1 counter-rotating turbine aiming to increase efficiency and apply constraints to mass flow rate and pressure ratio is taken. 展开更多
关键词 adjoint method aerodynamic shape optimization multi-stage turbomachinery N-S equations
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