首页 | 本学科首页   官方微博 | 高级检索  
文章检索
  按 检索   检索词:      
出版年份:   被引次数:   他引次数: 提示:输入*表示无穷大
  收费全文   217篇
  免费   129篇
  国内免费   23篇
  2024年   2篇
  2023年   2篇
  2022年   6篇
  2021年   8篇
  2020年   3篇
  2019年   1篇
  2018年   3篇
  2017年   15篇
  2016年   11篇
  2015年   15篇
  2014年   17篇
  2013年   13篇
  2012年   23篇
  2011年   12篇
  2010年   18篇
  2009年   23篇
  2008年   24篇
  2007年   14篇
  2006年   18篇
  2005年   11篇
  2004年   16篇
  2003年   10篇
  2002年   10篇
  2001年   17篇
  2000年   12篇
  1999年   7篇
  1998年   9篇
  1997年   5篇
  1996年   5篇
  1995年   6篇
  1994年   10篇
  1993年   4篇
  1992年   5篇
  1991年   5篇
  1990年   4篇
  1989年   3篇
  1988年   1篇
  1987年   1篇
排序方式: 共有369条查询结果,搜索用时 156 毫秒
361.
BBO晶体II型相位匹配光参量振荡器的输出线宽   总被引:1,自引:0,他引:1  
采用355nm脉冲激光作为泵浦源,对影响BBO晶体II型相位匹配光参量振荡器输出线宽的各种物理机制进行了数值模拟计算和分析。结果表明,II型相位匹配是光参量振荡器获得窄线宽的有效而简单的手段。  相似文献   
362.
通过对光电跟踪仪安装时水平度调整方法的研究,提出了利用坐标变换算法,用以实现光电跟踪仪安装时水平度的快速调整.利用该算法不但可以减少安装时的测量次数,节约安装调整时间,而且提高了设备安装时的测量精度,具有广泛的推广应用价值.文中还对该方法的测量计算误差进行了分析.  相似文献   
363.
根据风洞现场测控系统的特点,对风洞现场的电磁干扰测量方法和技术进行研究,并在风洞中进行试验,得到了相关的试验数据.通过对数据的分析可以得出:影响风洞现场测控系统的电磁干扰源主要是大功率变频装置,耦合途径为空间辐射和电源线传导.  相似文献   
364.
针对火炮性能测试时难于实时、准确测量炮口扰动的问题,提出了一种基于光电位置传感器(Position Sen-sitive Detector,PSD)的炮口扰动测试方法。采用光学杠杆、激光脉冲调制、高精度光电位置传感器、高速数据采集技术,以及所建立的PSD测量炮口角数学模型构建炮口角测量系统,可有效消除炮口闪光、外界自然光及蚊虫干扰,具有较高的灵敏度、精度和可靠性。  相似文献   
365.
基于舰载无人机对岸上目标的观测能力出发研究出的"理想观参",考虑各种因素对舰载无人机在任务区域飞行安全的影响,建立了地理通视性分析模型、地理可飞性分析模型、飞行可控性分析模型、弹道安全性分析模型和观参上限分析模型;综合上述模型,给出了舰载无人机可观测安全飞行空间,满足可观测安全飞行空间的观测参数即为当前环境下的"实用观参";根据本文模型研制的舰载无人机对岸射击观测辅助决策软件,实现了舰载无人机对岸射击观测的科学决策。  相似文献   
366.
This study investigates the ricochet behaviour of three different small-arms projectile types using a novel ricochet measuring device.The results can be used to estimate the danger potential of ricochets on shooting ranges.A ricochet is the change of direction and velocity of a projectile after impacting an oblique surface.This impact produces strong vibrations on a rigid plate.During this impact,flexural waves travel radially outwards from the point of impact.These waves are used to determine the properties of the impactor with accelerometers situated on the target surface.With the use of two measurement plates,one can produce a ricochet and detect the velocity at the same time.Accelerometers are suitable for accurate momentum measurements of single impacts.However,depending upon strike velocity and the impact angle,a ricochet can separate in multiple fragments after being deflected.From the operational safety perspective,these fragments need to be detected,as well.The approach of a coupled sensor concept was chosen to solve this problem.Thermographic sensors were additionally used to visualise the heat which is produced after pene-trating a rubber layer pasted in front of the steel target plate.With this approach one was able to detect the position of impact.The investigations showed that the measurement system performance is better with a multiple sensor design,which includes accelerometers for the velocity,impact strength and partly the position measurement,while the thermographic sensor was used for the position measurement and partly the momentum measurement.The investigated ammunition showed plausible fragmentation behaviour,and the results can already be used to estimate the danger potential of different ammunition types.Frangible projectiles fragment to small particles already after being deflected under a small angle.However,Full Metal Jacket projectiles with or without a steel core do not fragment under angles which are less than 5°.The objective of the paper is to demonstrate the possibility of measuring the complex ricochet me-chanics of small projectiles using standard accelerometers with the adequate signal processing approach.This measuring system is supported by an off the shelf thermographic camera.  相似文献   
367.
In this paper,a novel launch dynamics measurement system based on the photoelectric sensor pair is built.The actual muzzle time(i.e.a time duration that originates from the initial movement to the rocket's departure from the muzzle)and the muzzle velocity are measured.Compared with the classical methods,the actual muzzle time is obtained by eliminating the ignition delay.The comparative analysis method is proposed with numerical simulations established by the transfer matrix method for multibody systems.The experiment results indicate that the proposed measurement system can effectively measure the actual muzzle time and reduce the error of classical methods,which match well with the simulation results showing the launch dynamics model is reliable and helpful for further analysis and design of the MLRS.  相似文献   
368.
The U.S. system for procuring and utilizing deceased‐donor organs for transplantation has been studied and written about in many articles. The purpose of this paper is to examine the interactions between the elements that comprise this system, and point out improvement opportunities that may be affected through operations research/management techniques. The authors demonstrate the need for developing data‐driven and analytic tools. In fact, data is used to generate hypotheses and support claims throughout the paper. The paper also points out the need to fully leverage data that is available to researchers, and to seek data that is currently not deposited in a centralized archive.  相似文献   
369.
光学镀膜宽带膜厚监控系统   总被引:11,自引:0,他引:11       下载免费PDF全文
针对过去的宽带膜厚监控法必须依赖镀制前设定的目标透射率 (反射率 )的固有缺陷 ,提出了在蒸镀过程中及时拟合出所镀层的膜厚、色散系数 (折射率 )等参数 ,并据此不断修正目标透射率 (反射率 )的设想 ,从而从根本上克服过去的宽带膜厚监控法的固有缺陷。建立了基于修正膜层目标光谱特性的宽带膜厚监控系统 ,阐述了它的结构和工作原理。进行了稳定性实验及一系列镀膜监控实验 ,实验结果表明 ,该系统透射率的重复测量精度优于 2‰ ,膜厚监控精度较高 ,重复性好 ,各层的终点膜厚判定精度优于 1 %。  相似文献   
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号