全文获取类型
收费全文 | 427篇 |
免费 | 18篇 |
国内免费 | 29篇 |
专业分类
航空 | 195篇 |
航天技术 | 182篇 |
综合类 | 26篇 |
航天 | 71篇 |
出版年
2023年 | 4篇 |
2022年 | 7篇 |
2021年 | 7篇 |
2020年 | 10篇 |
2019年 | 7篇 |
2018年 | 6篇 |
2017年 | 8篇 |
2016年 | 9篇 |
2015年 | 3篇 |
2014年 | 18篇 |
2013年 | 30篇 |
2012年 | 14篇 |
2011年 | 18篇 |
2010年 | 17篇 |
2009年 | 28篇 |
2008年 | 37篇 |
2007年 | 14篇 |
2006年 | 14篇 |
2005年 | 21篇 |
2004年 | 9篇 |
2003年 | 8篇 |
2002年 | 10篇 |
2001年 | 11篇 |
2000年 | 6篇 |
1999年 | 4篇 |
1998年 | 11篇 |
1997年 | 5篇 |
1996年 | 6篇 |
1995年 | 11篇 |
1994年 | 8篇 |
1993年 | 4篇 |
1992年 | 10篇 |
1991年 | 4篇 |
1990年 | 3篇 |
1989年 | 8篇 |
1988年 | 4篇 |
1987年 | 6篇 |
1986年 | 4篇 |
1985年 | 8篇 |
1984年 | 12篇 |
1983年 | 9篇 |
1982年 | 9篇 |
1981年 | 13篇 |
1980年 | 2篇 |
1972年 | 2篇 |
1971年 | 4篇 |
1970年 | 2篇 |
1969年 | 2篇 |
1968年 | 1篇 |
1967年 | 1篇 |
排序方式: 共有474条查询结果,搜索用时 15 毫秒
101.
介绍了水下测试基阵机械扫描装置的设计实例,对基阵架的杆部连接进行了有限元分析。根据碳纤维杆的受力变形情况进行了无拉杆状态、有两根拉杆状态及有四根拉杆状态下的有限元分析,并对其进行了实验验证,为设计提供必要的理论支持。 相似文献
102.
Garmash V.R. Katsenelenbaum B.Z. Shaposhnikov S.S. Tioulpakov V.N. Vaganov R.B. 《Aerospace and Electronic Systems Magazine, IEEE》1998,13(10):39-41
Some wave beam peculiarities which usually are wasted are useful in wireless power transmission systems. These peculiarities-the focusing of the beam, the taper distribution of the radiating field, and the discontinuous antenna-are discussed 相似文献
103.
To realize the maximum potential of large series connected battery packs, the individual battery voltages should be maintained at fairly uniform values, i.e., the voltages should be equalized. The ramp type of electronic equalizer has proven to be very effective in performing this task since it offers the advantages of simplicity and convenience. However, to achieve maximum performance, it is necessary to understand how the circuit is affected by certain parameters. This is accomplished by defining the circuit sensitivity and using a simplified model to explain the relative effects of leakage inductance, frequency, and power level 相似文献
104.
Static and fatigue tests under compression
load were made on impacted AS4/PEEK and T300/913C graphite/epoxy with [45/90/-45/0]5S
stacking sequence. The comparison of the damage tolerance assessment for thermosetting and
thermoplastic composites shows that thermoplastics are more damage tolerant under
compression. Impacted thermoplastic composites have excellent compression-compression
fatigue behavior. The damage growth life is only a few percent of their total fatigue life
and no regular damage growth can be found. Some design principles for thermosetting
composite structures may still be used. 相似文献
105.
T. Takada R. Nakamura Y. Asano W. Baumjohann A. Runov M. Volwerk T.L. Zhang Z. Vörös K. Keika B. Klecker H. Rème E.A. Lucek C. Carr H.U. Frey 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(10):1585-1592
We examined two consecutive plasma sheet oscillation and dipolarization events observed by Cluster in the magnetotail, which are associated with a pseudo-breakup and a small substorm monitored by the IMAGE spacecraft. Energy input from the solar wind and an associated enhancement of the cross-tail current lead to current sheet thinning and plasma sheet oscillations of 3–5 min periods, while the pseudo-breakups occur during the loading phase within a spatially limited area, accompanied by a localized dipolarization observed by DSP TC1 or GOES 12. That is, the so-called “growth phase” is a preferable condition for both pseudo-breakup and plasma sheet oscillations in the near-Earth magnetotail. One of the plasma sheet oscillation events occurs before the pseudo-breakup, whereas the other takes place after pseudo-breakup. Thus there is no causal relationship between the plasma sheet oscillation events and pseudo-breakup. As for the contribution to the subsequent small substorm, the onset of the small substorm took place where the preceding plasma sheet oscillations can reach the region. 相似文献
106.
Some data obtained in the course of computer-aided simulation of a process of plane AMg6 alloy specimen rolling in the CAE-system MSC.SuperForm are presented. The influence of a real material structure upon the stress-strain state and the flow pattern of layers throughout the specimen height is taken into account. Also determined are the values of total pressure of metal on the rolls and a moment of rolling with the use of the isotropic and anisotropic finite element models (FEM) of specimens. 相似文献
107.
The concept of “space patrol” is considered, aimed at discovering and cataloging the majority of celestial bodies that constitute
a menace for the Earth [1, 2]. The scheme of “optical barrier” formed by telescopes of the space patrol is analyzed, requirements
to the observation system are formulated, and some schemes of sighting the optical barrier region are suggested (for reliable
detection of the celestial bodies approaching the Earth and for determination of their orbits). A comparison is made of capabilities
of electro-jet engines and traditional chemical engines for arrangement of patrol spacecraft constellation in the Earth’s
orbit. 相似文献
108.
D. Koc-San B.T. San V. Bakis M. Helvaci Z. Eker 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
Astronomical observatory site selection is a complex problem that involves evaluation of multiple factors from different sources. The aim of this study is to select the best possible candidates for astronomical observations sites using Multi-Criteria Decision Analysis integrated with Geographical Information Systems and remote sensing technologies. The study was implemented in the Antalya province of Turkey, which is convenient for astronomical site observatory facilities with its appropriate climate properties and weather conditions. Eleven factors (cloud cover, precipitable water, earthquake zones, geology, landslide inventory, active fault lines, Digital Elevation Model, city lights, mining activities, settlement areas, roads) were determined, splitting into three categories; meteorological, geographical and anthropogenic criteria. These factors were evaluated using Analytical Hierarchy Process method and the weights of criteria layers were determined. As a result, the most suitable areas were located extensively in western and eastern part of Antalya. This study offers a robust, accurate, cost and time effective procedure for preliminary site selection for astronomical observatory. However, for a final decision of the best location of astronomical observatory, site testing measurements and atmospheric seeing observations will be further required in these preliminary areas. 相似文献
109.
A recursive method for calculating decoupling zeroes in the linear multiconnected dynamic system based on the application
of matrix canonization techniques is proposed. Its essence is that the problem dimension is successively decreased and reduced
to finding eigenvalues of some matrix. The results obtained can be used to check controllability and observability as well
as to calculate uncontrollable and unobservable modes of the dynamic system. 相似文献
110.
Y. Wu S.G. Jin Z.M. Wang J.B. Liu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
The detection and repair of the cycle slip or gross error is a key step for high precision global positioning system (GPS) carrier phase navigation and positioning due to interruption or unlocking of GPS signal. A number of methods have been developed to detect and repair cycle slips in the last two decades through cycle slip linear combinations of available GPS observations, but such approaches are subject to the changing GPS sampling and complex algorithms. Furthermore, the small cycle slip and gross error cannot be completely repaired or detected if the sampling is quite longer under some special observation conditions, such as Real Time Kinematic (RTK) positioning. With the development of the GPS modernization or Galileo system with three frequencies signals, it may be able to better detect and repair the cycle slip and gross error in the future. In this paper, the cycle slip and gross error of GPS carrier phase data are detected and repaired by using a new combination of the simulated multi-frequency GPS carrier phase data in different conditions. Results show that various real-time cycle slips are completely repaired with a gross error of up to 0.2 cycles. 相似文献