全文获取类型
收费全文 | 7063篇 |
免费 | 8篇 |
国内免费 | 34篇 |
专业分类
航空 | 3624篇 |
航天技术 | 2558篇 |
综合类 | 32篇 |
航天 | 891篇 |
出版年
2021年 | 39篇 |
2019年 | 46篇 |
2018年 | 69篇 |
2014年 | 114篇 |
2013年 | 163篇 |
2012年 | 142篇 |
2011年 | 206篇 |
2010年 | 150篇 |
2009年 | 240篇 |
2008年 | 323篇 |
2007年 | 163篇 |
2006年 | 179篇 |
2005年 | 185篇 |
2004年 | 165篇 |
2003年 | 221篇 |
2002年 | 138篇 |
2001年 | 224篇 |
2000年 | 138篇 |
1999年 | 182篇 |
1998年 | 219篇 |
1997年 | 140篇 |
1996年 | 203篇 |
1995年 | 257篇 |
1994年 | 238篇 |
1993年 | 148篇 |
1992年 | 172篇 |
1991年 | 91篇 |
1990年 | 84篇 |
1989年 | 192篇 |
1988年 | 78篇 |
1987年 | 85篇 |
1986年 | 81篇 |
1985年 | 259篇 |
1984年 | 195篇 |
1983年 | 167篇 |
1982年 | 171篇 |
1981年 | 239篇 |
1980年 | 83篇 |
1979年 | 62篇 |
1978年 | 67篇 |
1977年 | 66篇 |
1976年 | 47篇 |
1975年 | 81篇 |
1974年 | 51篇 |
1973年 | 60篇 |
1972年 | 66篇 |
1971年 | 54篇 |
1970年 | 58篇 |
1969年 | 55篇 |
1967年 | 38篇 |
排序方式: 共有7105条查询结果,搜索用时 93 毫秒
251.
Van Der Wal J.C. Van Willigen D. 《IEEE transactions on aerospace and electronic systems》1982,(5):520-530
A hard limiter is a simple, yet highly efficient, RF signal sensor for VLF and LF navigation receivers. The observation reliability is used as the single quality criterion for the hard limiter if applied as a singlebit analog-to-digital converter (ADC). The effects of noise (Gaussian and atmospheric), nonsynchronous and synchronous interference, and dc offset on the observation reliability are described extensively. The single parameter determination Pobs is adequate for characterizing the polarity detector. This facilitates rank ordering of influences disturbing the signal and is a useful tool in optimizing digital tracking loops. The ?built-in? noise-censoring properties of the hard limiter in the presence of atmospheric noise are excellent. Therefore, three different atmospheric noise models are used in the determination of the observation reliability Pobs. Some ways for coping with other disturbances that potentially threaten the good performance of the hard limiter are suggested. 相似文献
252.
An improved power converter model is developed by combining the average and discrete modeling techniques. The parameter determination of the proposed discrete-average model is shown to be dependent on the type of duty cycle control law and the nature of the error processor used in the feedback loop. Furthermore, the paper pinpoints deficiencies of the conventional loop gain measurement technique which is widely used in industries. 相似文献
253.
A. L. Broadfoot B. R. Sandel D. E. Shemansky S. K. Atreya T. M. Donahue H. W. Moos J. L. Bertaux J. E. Blamont J. M. Ajello D. F. Strobel J. C. McConnell A. Dalgarno R. Goody M. B. McElroy Y. L. Yung 《Space Science Reviews》1977,21(2):183-205
The Voyager Ultraviolet Spectrometer (UVS) is an objective grating spectrometer covering the wavelength range of 500–1700 Å with 10 Å resolution. Its primary goal is the determination of the composition and structure of the atmospheres of Jupiter, Saturn, Uranus and several of their satellites. The capability for two very different observational modes have been combined in a single instrument. Observations in the airglow mode measure radiation from the atmosphere due to resonant scattering of the solar flux or energetic particle bombardment, and the occultation mode provides measurements of the atmospheric extinction of solar or stellar radiation as the spacecraft enters the shadow zone behind the target. In addition to the primary goal of the solar system atmospheric measurements, the UVS is expected to make valuable contributions to stellar astronomy at wavelengths below 1000 Å. 相似文献
254.
Paulikas G.A. Blake J.B. Imamoto S.S. 《IEEE transactions on aerospace and electronic systems》1975,(6):1138-1144
The Aerospace Corporation energetic electron-proton spectrometer operating on Applications Technology Satellite-6 (ATS-6) detects energetic electrons in four channels between 140 keV and greater than 32 MeV, and measures energetic protons in five energy channels between 2.3 and 80 MeV and energetic alpha particles in three channels between 9.4 and 94 MeV. After more than a year of operation in orbit, the experiment continues to return excellent data on the behavior of energetic magnetospheric electrons as well as information regarding the fluxes of solar protons and alpha particles. 相似文献
255.
Implementing the optimal Neyman-Pearson (NP) fusion rule in distributed detection systems requires the sensor error probabilities to be a priori known and constant during the system operation. Such a requirement is practically impossible to fulfil for every resolution cell in a multiflying target multisensor environment. The true performance of the fusion center is often worse than expected due to fluctuations of the observed environment and instabilities of sensor thresholds. This work considers a nonparametric data fusion situation in which the fusion center knows only the number of the sensors, but ignores their error probabilities and cannot control their thresholds. A data adaptive approach to the problem is adopted, and combining P reports from Q independent distributed sensors through a least squares (LS) formulation to make a global decision is investigated. Such a fusion scheme does not entail strict stationarity of the noise environment nor strict invariance of the sensor error probabilities as is required in the NP formulation. The LS fusion scheme is analyzed in detail to simplify its form and determine its asymptotic behavior. Conditions of performance improvement as P increases and of quickness of such improvement are found. These conditions are usually valid in netted radar surveillance systems. 相似文献
256.
This paper presents a computational method for the calculation of probability of detection using measured radar target cross-section data. The described method can also be used for probability of detection calculations when the radar target cross section follows a specified probability density function. Using the computational procedure of the paper, a number of curves are generated which can be used for probability of detection calculations with exponential and Gaussian radar target cross-section distributions. The results obtained using theoretical distributions are compared with the corresponding results using actual target cross-section measurements. The results of computer runs are compared to the corresponding values in the literature where available. 相似文献
257.
The determination of the range of radar is carried out according to statistical methods which are not always immediate. For this reason, a parametrical method is proposed which condenses the elements necessary for this calculation in the form of three abaci. Furthermore, a general formula condenses this result, and the formula is extended to the other transmission systems. 相似文献
258.
A position fix in a passive mode using satellites usually necessitates an expensive computer or lengthy hand calculation. This is the largest drawback of passive navigation and it would be more desirable if the user could find his position by a mere glance at a chart and table, as one uses Loran. The first step toward this goal is to use a synchronous satellite because it simplifies the problem. The next step is to find the position of the user by a Loran type of chart, which is universal, and correct this apparent position by looking at a special table which is made according to the amount of perturbation of both the satellite and the user's position. An example of the position fix along the route between Yokohama to Hawaii is shown. The concept can be extended to orbiting satellites due to the rules which govern the motion of satellites, if the fix accuracy is in the order of 2 to 5 miles. This method should be more accurate than the common sextant and more practical due to the fact that the satellite can be used at any time and in any weather. As a total system, it will be better than Omega because it could provide additional navigation information such as communication or traffic control by using satellites. 相似文献
259.
An expression is derived for the cost resultingfrom the stabilization of a satellite using aspecific optimal control (SOC). An exampleis given in which the optimal and SOC yieldvirtually identical costs. 相似文献
260.
R. J. Murphy 《Space Science Reviews》2007,130(1-4):127-138
Interactions of ions accelerated in solar flares produce gamma-ray lines and continuum and neutrons. These emissions contain
a rich set of observables that provides information about both the accelerated ions and the environment where the ions are
transported and interact. Ion interactions with the various nuclei present in the ambient medium produce gamma-ray lines at
unique energies. How abundance information is extracted from the measurements is discussed and results from analyses of a
number of solar flares are presented. The analyses indicate that the composition of the ambient gas where the ions interact
(typically at chromospheric densities) is different from that of the photosphere and more like the composition of the corona,
exhibiting low-FIP elemental enhancements that may vary from flare to flare. Evidence for increased Ne/O and the photospheric
3He abundance is also discussed. 相似文献