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   6021篇
  免费   38篇
  国内免费   18篇
航空   2741篇
航天技术   2139篇
综合类   24篇
航天   1173篇
  2021年   62篇
  2019年   41篇
  2018年   147篇
  2017年   111篇
  2016年   101篇
  2015年   49篇
  2014年   170篇
  2013年   179篇
  2012年   184篇
  2011年   280篇
  2010年   190篇
  2009年   315篇
  2008年   375篇
  2007年   184篇
  2006年   144篇
  2005年   181篇
  2004年   162篇
  2003年   203篇
  2002年   132篇
  2001年   195篇
  2000年   96篇
  1999年   125篇
  1998年   155篇
  1997年   121篇
  1996年   115篇
  1995年   157篇
  1994年   145篇
  1993年   94篇
  1992年   124篇
  1991年   63篇
  1990年   50篇
  1989年   114篇
  1988年   51篇
  1987年   52篇
  1986年   45篇
  1985年   142篇
  1984年   126篇
  1983年   104篇
  1982年   115篇
  1981年   155篇
  1980年   65篇
  1979年   45篇
  1978年   47篇
  1977年   33篇
  1976年   42篇
  1975年   36篇
  1974年   30篇
  1973年   29篇
  1972年   28篇
  1971年   28篇
排序方式: 共有6077条查询结果,搜索用时 266 毫秒
951.
In many domestic satellite communication systems single-channel per-carrier FM (SCPC-FM) has become the accepted transmission method for thin route communication. The SCPC-FM modem operates over a wide range of carrier frequencies and is designed to use satellite power and bandwidth efficiently. It incorporates elements which make the signal transfer complex, so the system behavior is not immediately obvious. This article investigates the signal processes and analyzes the performance of a companded and preemphasized SCPC-FM system and it furnishes insight into the choice of crucial system parameters.  相似文献   
952.
The USSR has always been reluctant to reveal details of failures in its space programme, and only a few failures have been annouced publically. Some official US sources list failures in the Soviet programme, although these official listings end in mid-1964. The aviation press often reports rumoured failures, and it is the job of an analyst to try and separate the wheat from the chaff.  相似文献   
953.
954.
In this review, current state of knowledge of high resolution observations at decameter wavelengths of the quiet Sun, the slowly varying component (SVC), type I to V bursts and noise storms is summarized. These observations have been interpreted to yield important physical parameters of the solar corona and the dynamical processes around 2R from the photosphere where transition from closed to open field lines takes places and the solar wind builds up. The decametric noise bursts have been classified into (i) BF type bursts which show variation of intensity with frequency and time and (ii) decametric type III bursts. The angular sizes of noise storm sources taking into account refraction and scattering effects are discussed. An attempt has been made to give phenomenology of all the known varieties of decametric bursts in this review. Available polarization information of decametric continuum and bursts has been summarized. Recent simultaneous satellite and ground-based observations of decametric solar bursts show that their intensities are deeply modulated by scintillations in the Earth's ionosphere. Salient features of various models and theories of the metric and decametric noise storms proposed so far are examined and a more satisfactory model is suggested which explains the BF type bursts as well as conventional noise storm bursts at decametric wavelengths invoking induced scattering process for 1 t conversion. Some suggestions for further solar decametric studies from the ground-based and satellite-borne experiments have been made.  相似文献   
955.
The defruiter that is employed in the Air Traffic Control Radar Beacon System (ATCRBS) to prefilter asynchronous replies has a complex impact on the detection, estimation and validation properties of the detection subsystem. Its positive and negative effects are quantitatively enumerated via a simulation of the beacon processing subsystem of the Automated Radar Terminal System (ARTS III). It is concluded that the disadvantages of using the present-day defruiter in the ARTS III digital processing channel outweigh the advantages when fruit rates are below several thousand per scan. As an alternative to the total elimination of the defruiter a more general class of preprocessors is defined and their input-output relationships are derived using a Markov Chain formulation. These are found to represent an improvement over the current defruiter in that the positive effects of defruiting are retained while some of the negative effects are reduced.  相似文献   
956.
957.
Accurate solutions of minimal time Earth-Mars and Earth-Venus heliocentric trajectories are calculated with a shooting-Newton method. The flight times are less and the steering histories are diferent than those presented in [1], thus contradicting the optimality claims in [1].  相似文献   
958.
The Langmuir-probe technique for measurement of electron concentration in the mesosphere is capable of excellent altitude resolution, of order 1 m. Measurements from nine rocket flights frequently show small-scale ionization structures in the altitude region 60–90 km. These are believed to be identical with regions of strong coherent backscatter seem by VHF radars at Jicamarca, Peru and Urbana, Illinois. They are believed to represent intermittent turbulence attributable to nonlinear interaction of waves in the mesosphere. Parameters of the turbulent regions are estimated.  相似文献   
959.
The problem considered in this paper is the investigation of the properties of a mass-meter, i.e. the device for determining the mass of cosmonaut's body under zero-gravity conditions. The estimates of accuracy of mass measurement by this device are given, and the results of measuring the masses of cosmonauts' bodies on the Salyut 5 and 6 orbital stations are presented.  相似文献   
960.
The environment and radar operation simulator (EROS) is a hardware system whose function is to produce realistic synthetic radar backscatter, incorporating both target and clutter. The simulator is electrically connected to a subject radar and responds in real time to the radar's antenna scan angle by producing the correct composite video signal.  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