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   3711篇
  免费   9篇
  国内免费   9篇
航空   1668篇
航天技术   1339篇
综合类   183篇
航天   539篇
  2021年   22篇
  2019年   24篇
  2018年   69篇
  2017年   38篇
  2016年   40篇
  2015年   22篇
  2014年   85篇
  2013年   102篇
  2012年   82篇
  2011年   136篇
  2010年   78篇
  2009年   154篇
  2008年   184篇
  2007年   101篇
  2006年   99篇
  2005年   99篇
  2004年   101篇
  2003年   114篇
  2002年   166篇
  2001年   172篇
  2000年   58篇
  1999年   93篇
  1998年   103篇
  1997年   82篇
  1996年   107篇
  1995年   121篇
  1994年   92篇
  1993年   55篇
  1992年   84篇
  1991年   32篇
  1990年   28篇
  1989年   71篇
  1988年   30篇
  1987年   26篇
  1986年   31篇
  1985年   118篇
  1984年   107篇
  1983年   63篇
  1982年   92篇
  1981年   117篇
  1980年   29篇
  1978年   27篇
  1977年   27篇
  1976年   20篇
  1975年   21篇
  1974年   26篇
  1972年   25篇
  1971年   22篇
  1970年   23篇
  1969年   25篇
排序方式: 共有3729条查询结果,搜索用时 10 毫秒
801.
Coherent high-resolution synthetic-aperture radar systems achieve their range resolution by pulse compression and azimuth resolution by compression of naturally generated FM coding due to Doppler shifts as the aircraft flies by the target. If the data is left unprocessed, it is, in effect, a defocused map of the terrain. As such, it should exhibit less dynamic range than if the data is compressed. This paper describes an experimental study to verify the above conjecture. The results of this study indicate that if dynamic range of the data link is a problem, the radar data should be transmitted in its unprocessed form. This might very well be the case for planetary mapping by means of satellites.  相似文献   
802.
This paper develops, in a unique manner, a numeric algorithm for an integration and extrapolation scheme. The purpose of presenting it in this manner is to develop in the reader a complete understanding of how the algorithm is derived. It is also intended to give an insight into the limitations of the algorithm and to serve as a tool to derive additional integration schemes.  相似文献   
803.
Problems of improving the efficiency of design works in the process of space-rocket complex (SRC) updating are considered. The methodical foundation for the expert system application to form promising technical solutions in studying the flight vehicle (FV) modification is presented.  相似文献   
804.
805.
This paper presents a literature survey on the recent developments related to experimental and modeling studies of transient luminous events (TLEs) in the middle atmosphere termed elves, sprites and jets that are produced in association with thunderstorm activity at tropospheric altitudes. The primary emphasis is placed on publications that appeared in refereed literature starting from year 2008 and up to the present date. The survey covers general phenomenology of TLEs and their relationships to characteristics of individual thunderstorms and lightning, physical mechanisms and modeling of TLEs, past, present and future orbital observations of TLEs, and their chemical, energetic and electric effects on local and global scales.  相似文献   
806.
We describe the design, performance and scientific objectives of the NASA-funded ALICE instrument aboard the ESA Rosetta asteroid flyby/comet rendezvous mission. ALICE is a lightweight, low-power, and low-cost imaging spectrograph optimized for cometary far-ultraviolet (FUV) spectroscopy. It will be the first UV spectrograph to study a comet at close range. It is designed to obtain spatially-resolved spectra of Rosetta mission targets in the 700–2050 Å spectral band with a spectral resolution between 8 Å and 12 Å for extended sources that fill its ~0.05^ × 6.0^ field-of-view. ALICE employs an off-axis telescope feeding a 0.15-m normal incidence Rowland circle spectrograph with a toroidal concave holographic reflection grating. The microchannel plate detector utilizes dual solar-blind opaque photocathodes (KBr and CsI) and employs a two-dimensional delay-line readout array. The instrument is controlled by an internal microprocessor. During the prime Rosetta mission, ALICE will characterize comet 67P/Churyumov-Gerasimenko's coma, its nucleus, and nucleus/coma coupling; during cruise to the comet, ALICE will make observations of the mission's two asteroid flyby targets and of Mars, its moons, and of Earth's moon. ALICE has already successfully completed the in-flight commissioning phase and is operating well in flight. It has been characterized in flight with stellar flux calibrations, observations of the Moon during the first Earth fly-by, and observations of comet C/2002 T7 (LINEAR) in 2004 and comet 9P/Tempel 1 during the 2005 Deep Impact comet-collision observing campaign.  相似文献   
807.
In digital communication systems, optimum estimation and detection algorithms require that precise knowledge of the bit transition time be known to the receiver before bit-by-bit detection can be made. This paper presents the derivation of Bayes or maximum a posteriori estimation algorithms for optimum estimation of bit timing. Performance of the optimum system is evaluated and suboptimal realizations suggested.  相似文献   
808.
In angle tracking antenna applications, the angle sensing boresight accuracy capabilities are important. The ability of an antenna to precisely determine the bearing angle to a point source is determined by the slope of the control function pattern at boresight. In the presence of extraneous interference, the magnitudes of the sidelobe and backlobe responses are important. Control pattern slope (angular sensitivity) is primarily a function of aperture illumination. It can be described by a current distribution in intensity and phase at every point. Once distribution is defined, lobe structure is defined by the associated transform. When more than one feed is used, the distribution will be a vector sum of the individual feed distributions. The resulting secondary pattern can be defined in terms of the amplitude distribution and the phase center locations of the contributing feeds. With a four-horn monopulse configuration, the feed phase centers are displaced from the boresight axis. Placing the phase centers on the boresight axis by rotating the feeds through 45 degrees results in a different set of intensity and phase values. A quite different secondary pattern results. The control function obtained by the subtraction of the powers from a paired set of on-axis feeds results in a lower sidelobe level than that obtained with a conventional monopulse combiner for a given feed taper.  相似文献   
809.
A detailed account is given of the application of a minimizationprogram to several design problems. Specifically these applications areconcerned with the design of a curve function generator for a massspectrometer for a proposed Mars probe and the design of autonomousshift registers with linear and nonlinear feedback, used for classificationion of binary sequences and counting tasks for spacecraft scientificdata processing.  相似文献   
810.
科技综合实力评估指标与数学模型   总被引:10,自引:0,他引:10  
运用灰色系统原理和德尔菲法,建立了省级区域科技综合实力评估指标体系。在灰色定权聚类模型的基础上,提出了一种基于三角白化权函数的评估模型。  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