全文获取类型
收费全文 | 366篇 |
免费 | 152篇 |
国内免费 | 29篇 |
出版年
2024年 | 4篇 |
2022年 | 5篇 |
2021年 | 17篇 |
2020年 | 9篇 |
2019年 | 8篇 |
2018年 | 6篇 |
2017年 | 22篇 |
2016年 | 24篇 |
2015年 | 13篇 |
2014年 | 30篇 |
2013年 | 39篇 |
2012年 | 25篇 |
2011年 | 31篇 |
2010年 | 19篇 |
2009年 | 34篇 |
2008年 | 34篇 |
2007年 | 30篇 |
2006年 | 24篇 |
2005年 | 29篇 |
2004年 | 20篇 |
2003年 | 19篇 |
2002年 | 16篇 |
2001年 | 14篇 |
2000年 | 5篇 |
1999年 | 10篇 |
1998年 | 12篇 |
1997年 | 6篇 |
1996年 | 5篇 |
1995年 | 2篇 |
1994年 | 5篇 |
1993年 | 5篇 |
1992年 | 2篇 |
1991年 | 4篇 |
1990年 | 17篇 |
1989年 | 2篇 |
排序方式: 共有547条查询结果,搜索用时 46 毫秒
211.
Curtis H. Martin 《The Nonproliferation Review》2013,20(1):61-88
Scholarly and popular literature in the recent past has framed nonproliferation diplomacy toward both Iran and North Korea as an example of “good cop/bad cop,” a social-psychological strategy borrowed from law enforcement to describe a process for forcing a confession by subjecting a target to stressful emotional contrast. This article examines those two cases, roughly covering the period since 2003, when the most recent attempts to deal with the Iranian and North Korean proliferation threats began, in light of criteria for employment of the good cop/bad cop strategy. There is some evidence that within the framework of the six-party talks with North Korea and within the framework of the EU-3-U.S. diplomacy toward Iran, the players seeking nonproliferation have adopted good cop/bad cop roles to that end. The article concludes, however, that while there are similarities to the interrogation room technique, the complexity of the international political environment as compared to the interrogation room has prevented the states involved from successfully adopting or effectively exploiting good and bad cop roles. Substantial and exploitable differences of interest among them, and the availability of alternative “escape routes” for the target state, raise serious questions about the applicability of the good cop/bad cop strategy to these two nonproliferation cases, and even about its applicability in future nonproliferation challenges. 相似文献
212.
反舰导弹(矛)与舰载反导武器(盾)之间的斗争是现代海战重要格局之一。美俄二大军事大国在矛与盾的发展上,均以对方为假想敌,研究使自己的矛如何突防对方的盾,以及自己的盾如何拦击对方的矛。由于历史条件,国家政治需要和本国的技术优势不同,二国发展矛与盾的指导思想和设计准则,以及在攻防策略上都有很大不同。文章从深层次分析这些不同特点,并探讨它们的发展走向。 相似文献
213.
214.
为了提高无人机自主飞行、自主攻击的能力,设计一种整体式的无人机综合火力/飞行控制系统(IFFC系统),并对激光制导炸弹模态下的系统进行数字仿真.系统基于Winsock的TCP/IP协议的C/S模式,在服务器上完成无人机火控解算、火飞耦合器设计,在客户端设计基于PID算法的飞行控制模块.火控系统根据飞行状态和目标信息实时计算炸弹可达区域,瞄准距离误差经过火飞耦合器形成航向和俯仰控制命令反馈给飞控系统,驱动载机消.除瞄准误差,实现闭环控制.实验结果表明,无人机的瞄准速度和攻击精度都有所提高,为进一步开展自主式UAV的研究打下基础. 相似文献
215.
The effects of magnesium/polytetrafluoroethylene (Mg/PTFE) pyrotechnic compositions on the coupled flow field and reignition mechanism are important aspects governing the performance and range of base bleed projectiles (BBPs).Owing to a decrease in pressure and temperature when the BBP leaves the muzzle,rapid depressurization occurs,which extinguishes the base bleed propellant.The Mg/PTFE py-rotechnic composition pressed in the igniter of the base bleed unit (BBU) provides additional energy to the BBU via a chemical reaction.Thus,the extinguished base bleed propellant is reignited under the effect of high-temperature combustion gas jets from the igniter.In this study,a numerical analysis is conducted to evaluate the effects of PTFE and Mg granularity as well as Mg/PTFE pyrotechnic compo-sitions.Owing to the rapid depressurization,the temperature and pressure was found to decrease for different Mg/PTFE pyrotechnic compositions.However,the depressurization time increased as the PTFE granularity increased,the Mg granularity decreased,and the Mg content increased.When the pressure in the combustion chamber of the BBU decreased to the atmospheric pressure,the combustion gas jets from the igniter expand upstream (rather than downstream).However,these combustion gas jets exhibit different axial and radial expansion characteristics depending on the pyrotechnic compositions used.The results show that the reignition delay time,td,of the base bleed propellant was 377.608,94.27,387.243,523.966,and 221.094 ms for cases A-E,respectively.Therefore,it was concluded that the Mg/PTFE pyrotechnic composition of case B was the most beneficial for the reignition of the base bleed propellant,with the earliest addition of energy and mass to the BBP. 相似文献
216.
217.
Antoon W.J. Kolen Jan Karel Lenstra Christos H. Papadimitriou Frits C.R. Spieksma 《海军后勤学研究》2007,54(5):530-543
In interval scheduling, not only the processing times of the jobs but also their starting times are given. This article surveys the area of interval scheduling and presents proofs of results that have been known within the community for some time. We first review the complexity and approximability of different variants of interval scheduling problems. Next, we motivate the relevance of interval scheduling problems by providing an overview of applications that have appeared in literature. Finally, we focus on algorithmic results for two important variants of interval scheduling problems. In one variant we deal with nonidentical machines: instead of each machine being continuously available, there is a given interval for each machine in which it is available. In another variant, the machines are continuously available but they are ordered, and each job has a given “maximal” machine on which it can be processed. We investigate the complexity of these problems and describe algorithms for their solution. © 2007 Wiley Periodicals, Inc. Naval Research Logistics, 2007 相似文献
218.
为适应深空探测的应用需求,全球卫星导航系统对深空飞行器定位的可行性问题备受关注。针对探月飞行器月球公转轨道上的GNSS定位问题,以高轨道飞行器GNSS定位的研究为基础,采用多系统联合定位的方法进行仿真。分析了载波功率与噪声功率密度比为15dB-Hz的弱信号捕获门限下,各系统联合定位时波束主瓣和旁瓣的可用性,同时对各系统联合情况下的精度因子值进行分析。仿真结果表明:当接收到的卫星天线辐射的主瓣和旁瓣信号均高于载噪比门限时,全球卫星导航系统的三系统或四系统的联合能满足实时定位条件;而旁瓣损耗不加以补偿时,接收信号载噪比低于门限并导致任意联合方式均无法完成定位。各系统联合的精度因子分析表明:单系统或双系统联合的几何精度因子变化剧烈,四系统联合相比三系统联合的几何精度因子下降16.93%;三系统联合定位方案中,美国全球定位系统、中国的北斗卫星导航定位系统与欧洲的伽利略卫星导航定位系统联合方案的几何精度因子值变化最平稳,为最佳选择。理论分析和仿真结果为探月飞行器定位技术研究和星载多系统接收机设计提供参考。 相似文献
219.
运用冲击波理论,对横向效应增强型弹丸(Penetration with Enhanced Lateral Efficiency,PELE)侵穿金属靶板的机理进行了分析,将PELE侵彻过程中能量损失分为外壳和内芯撞击靶板区域环形塞块获得的能量,冲击波影响范围内外壳和内芯增加的内能,外壳前端外沿和内沿对靶板冲塞剪切耗能等,给出了确定这些能量的计算方法;并依据能量守恒原理,给出了PELE正撞金属薄靶板靶后剩余速度的近似计算公式。公式计算结果与多种条件下实验结果均吻合较好。分析计算所得各能量损失结果表明,弹体内芯材料的变化对弹体侵彻能力的影响较小;侵彻中靶板塞块获得的能量在弹体侵彻动能损失中比重最大;外壳前端内沿对靶板的剪切能耗对弹体动能损失的影响可以忽略。 相似文献
220.