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   11387篇
  免费   1202篇
  国内免费   1296篇
航空   6259篇
航天技术   3519篇
综合类   1140篇
航天   2967篇
  2023年   36篇
  2022年   134篇
  2021年   194篇
  2020年   196篇
  2019年   138篇
  2018年   238篇
  2017年   199篇
  2016年   209篇
  2015年   287篇
  2014年   500篇
  2013年   528篇
  2012年   624篇
  2011年   710篇
  2010年   693篇
  2009年   787篇
  2008年   817篇
  2007年   621篇
  2006年   508篇
  2005年   497篇
  2004年   383篇
  2003年   397篇
  2002年   352篇
  2001年   407篇
  2000年   337篇
  1999年   402篇
  1998年   406篇
  1997年   323篇
  1996年   270篇
  1995年   281篇
  1994年   314篇
  1993年   212篇
  1992年   244篇
  1991年   176篇
  1990年   128篇
  1989年   180篇
  1988年   105篇
  1987年   96篇
  1986年   62篇
  1985年   107篇
  1984年   102篇
  1983年   83篇
  1982年   98篇
  1981年   125篇
  1980年   43篇
  1979年   36篇
  1978年   32篇
  1977年   25篇
  1976年   28篇
  1973年   23篇
  1972年   23篇
排序方式: 共有10000条查询结果,搜索用时 68 毫秒
911.
一种新颖的瞬时浮点放大器   总被引:2,自引:0,他引:2  
介绍了瞬时浮点放大器的原理及构成,并给出一种结构新的具有256阶的瞬时浮点放大器,可有效地提高数据采集系统的测量范围。  相似文献   
912.
基于抓持稳定度的多指灵巧手抓持控制   总被引:6,自引:0,他引:6  
提出了一种控制多指灵巧手稳定抓持物体的新方法。首先给出了接触稳定度和抓持稳定度的定义及其相应的计算方法,然后探讨了基于抓持稳定度的多指灵巧手抓持控制方法。最后以北京航空航天大学的BH-2新型三指灵巧手为背景,对所提出的方法进行了仿真验证,仿真结果证明所提方法是有效可行的。  相似文献   
913.
研究了截除低载对全机结构各部位裂纹扩展寿命的影响,导出寿命误差与裂纹扩展比的关系,并指出寿命误差主要取决于开裂结构的材料参数,而开裂部位的影响则可忽略不计。  相似文献   
914.
本文介绍了某直升机电子特设系统综合模拟试验的直升机运动仿真模型,在此基础上着重对直升机航姿信号两种仿真方法进行了详细的阐述,并对两种方法的仿真试验结果进行了分析比较,指出了各自的优缺点。  相似文献   
915.
Capturability of the pure proportional navigation (PPN) guidance law against a target executing bounded piecewise continuous time-varying manoeuvres is investigated. A qualitative analysis is carried out to obtain a set of sufficient conditions for capture defined on the engagement parameters and initial conditions. These conditions are significantly less restrictive than the ones obtained previously by others using the Lyapunov method. It is shown that the actual capture region for time-varying target manoeuvres, obtained by using the conditions derived, is much larger than that obtained from the Lyapunov technique. We also show that though a bounded tine varying target manoeuvre does change the constant target manoeuvre capture region to some extent, it does not reduce it drastically. Further, we show that the worst case capture region is obtained when the target executes a constant manoeuvre equal to the bound on the manoeuvre level. Some bounds on the missile lateral acceleration are also obtained for certain regions in the engagement plane. These results are generalizations and extensions of existing results on the capturability of the PPN guidance law against targets executing constant or time-varying target manoeuvres  相似文献   
916.
本文阐述了媒体素材的采集及处理方法 ,对现代远程教育工程建设可提供有效的帮助  相似文献   
917.
Messenger  S.  Stadermann  F.J.  Floss  C.  Nittler  L.R.  Mukhopadhyay  S. 《Space Science Reviews》2003,106(1-4):155-172
Interplanetary dust particles collected in the stratosphere frequently exhibit enrichments in deuterium (D) and 15N relative to terrestrial materials. These effects are most likely due to the preservation of presolar interstellar materials. While the elevated D/H ratios probably resulted from mass fractionation during chemical reactions at very low < 100 K temperatures, the origin of the N isotopic anomalies remains unresolved. The bulk of the N-bearing material may have obtained its isotopic signatures from low temperature chemistry, but a nucleosynthetic origin is also possible. This revised version was published online in August 2006 with corrections to the Cover Date.  相似文献   
918.
919.
Feng  Xueshang  Wu  S.T.  Wei  Fengsi  Fan  Quanlin 《Space Science Reviews》2003,107(1-2):43-53
It has been believed that three-dimensional, numerical, magnetohydrodynamic (MHD) modelling must play a crucial role in a seamless forecasting system. This system refers to space weather originating on the sun; propagation of disturbances through the solar wind and interplanetary magnetic field (IMF), and thence, transmission into the magnetosphere, ionosphere, and thermosphere. This role comes as no surprise to numerical modelers that participate in the numerical modelling of atmospheric environments as well as the meteorological conditions at Earth. Space scientists have paid great attention to operational numerical space weather prediction models. To this purpose practical progress has been made in the past years. Here first is reviewed the progress of the numerical methods in solar wind modelling. Then, based on our discussion, a new numerical scheme of total variation diminishing (TVD) type for magnetohydrodynamic equations in spherical coordinates is proposed by taking into account convergence, stability and resolution. This new MHD model is established by solving the fluid equations of MHD system with a modified Lax-Friedrichs scheme and the magnetic induction equations with MacCormack II scheme for the purpose of developing a combined scheme of quick convergence as well as of TVD property. To verify the validation of the scheme, the propagation of one-dimensional MHD fast and slow shock problem is discussed with the numerical results conforming to the existing results obtained by the piece-wise parabolic method (PPM). Finally, some conclusions are made. This revised version was published online in August 2006 with corrections to the Cover Date.  相似文献   
920.
Langmuir waves and turbulence resulting from an electron beam-plasma instability play a fundamental role in the generation of solar radio bursts. We report recent theoretical advances in nonlinear dynamics of Langmuir waves. First, starting from the generalized Zakharov equations, we study the parametric excitation of solar radio bursts at the fundamental plasma frequency driven by a pair of oppositely propagating Langmuir waves with different wave amplitudes. Next, we briefly discuss the emergence of chaos in the Zakharov equations. We point out that chaos can lead to turbulence in the source regions of solar radio emissions. This revised version was published online in August 2006 with corrections to the Cover Date.  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