全文获取类型
收费全文 | 3180篇 |
免费 | 8篇 |
国内免费 | 9篇 |
专业分类
航空 | 1683篇 |
航天技术 | 1087篇 |
综合类 | 9篇 |
航天 | 418篇 |
出版年
2018年 | 37篇 |
2017年 | 19篇 |
2016年 | 23篇 |
2014年 | 56篇 |
2013年 | 81篇 |
2012年 | 59篇 |
2011年 | 106篇 |
2010年 | 82篇 |
2009年 | 113篇 |
2008年 | 179篇 |
2007年 | 90篇 |
2006年 | 60篇 |
2005年 | 77篇 |
2004年 | 78篇 |
2003年 | 100篇 |
2002年 | 52篇 |
2001年 | 100篇 |
2000年 | 48篇 |
1999年 | 79篇 |
1998年 | 93篇 |
1997年 | 73篇 |
1996年 | 91篇 |
1995年 | 126篇 |
1994年 | 99篇 |
1993年 | 66篇 |
1992年 | 101篇 |
1991年 | 42篇 |
1990年 | 36篇 |
1989年 | 87篇 |
1988年 | 34篇 |
1987年 | 29篇 |
1986年 | 33篇 |
1985年 | 88篇 |
1984年 | 93篇 |
1983年 | 60篇 |
1982年 | 86篇 |
1981年 | 92篇 |
1980年 | 35篇 |
1979年 | 43篇 |
1978年 | 32篇 |
1977年 | 22篇 |
1976年 | 21篇 |
1975年 | 37篇 |
1974年 | 24篇 |
1973年 | 18篇 |
1972年 | 29篇 |
1969年 | 17篇 |
1968年 | 16篇 |
1967年 | 20篇 |
1966年 | 16篇 |
排序方式: 共有3197条查询结果,搜索用时 15 毫秒
121.
US Army helicopters that will allow single-crewmember operability in tactical environments require a high degree of automation. A tightly integrated flight control and navigation system has been studied. An architecture is discussed which meets anticipated flight control and navigation requirements, at an acceptable weight, using techniques of functional and physical integration. The architecture maximizes the sharing of sensor and computational resources in a flight critical environment and uses modular equipment packaging, dual fault-tolerant tetrad ring-laser-gyro inertial measurement units, and triplex self-checking processor pair-based flight critical processing channels 相似文献
122.
A.H. Manson C.E. Meek K. Labitzke 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1984,4(4):51-55
The global developments of the stratospheric events (~20–50 km) are briefly described using balloon and satellite data. Winds data from L.F. drift (52°N, 15°E, Europe) for heights of 90–100 km, and from M.F. radar (52°N, 107°W, Canada) for heights of 60–110 km are then compared with the stratospheric morphology.Data for 1982/3 and 1983/4 show that the planetary wave activity and warmings produced strong westward and southward perturbations in the radar winds. Satellite data from 0.1, 0.01 hPa are consistent with these winds; and also show smaller scale structures in the mesosphere than the stratosphere. The semi-diurnal tide responded strongly to the atmospheric disturbances in Europe and Canada: for the latter vertical wavelength changes occurred for heights of 70–100 km. However the correlation between these tidal fluctuations was not high indicating that the tidal adjustments were continental rather than hemispheric. 相似文献
123.
V.C. Liu 《Progress in Aerospace Sciences》1975,16(3):273-297
This paper presents theoretical methods to determine the gas dynamic and the electrostatic effects due to the interaction caused by a rapidly moving body in the ionosphere. The principles of the methods are derived from the kinetic theory of collision-free plasma. It is shown that the collective behavior of the collision-free plasma makes it possible to use the fluid approach to treat the problems of ionospheric aerodynamics. Various solutions to the system of fluid and field equations that have direct bearing on the ionospheric aerodynamics are presented and discussed. Physical significances of the mathematical results are stressed. Some outstanding unsolved problems in ionospheric aerodynamics are elaborated and discussed. 相似文献
124.
The author describes his experiences in the early days in radar, working on a radar landing system called ground control approach (GCA). He discusses for the disparity between the short time from conception to worldwide deployment of that system and today's 10- to 15-year cycle, as well as GCA's high (100%) availability, and identifies the factors responsible. The author goes on to argue that the radar community has a history of overselling what radar can do. He forecasts future trends and concludes with a few things he has learned over the years 相似文献
125.
Buongiorno C. Vallerani E. Borriello G. 《Aerospace and Electronic Systems Magazine, IEEE》1989,4(5):17-25
The authors present the plan under discussion in Italy between the government entities and Aeritalia, the leading Italian aerospace company, for the technology development needed to support advanced transportation systems. The plan centers around the following areas: thermal protection and control; advanced structures and materials; guidance, navigation, and control; and tests and computation methods. Experimental activities needed to support the development of such systems and the difficulties involved are examined 相似文献
126.
T.C. Forbes 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1984,4(7):53-56
The resistive MHD equations are numerically solved in two dimensions for an initial-boundary-value problem which simulates reconnection between an emerging magnetic flux region and an overlying coronal magnetic field. The solution involves both ideal-MHD and resistive-MHD processes, and the solution shows an evolution which is remarkably suggestive of the preflare, impulsive, and main phases of the flare-cycle. 相似文献
127.
128.
J.W. Harvey 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1982,2(11):31-37
The decaying solar active region that crossed the central meridian on May 20, 1980 at latitude S13° produced a major flare (2B/X1) at 2054 on May 21. This region was a target of the international Flare Buildup Study and was well observed. The buildup was characterized by little flare activity during two days prior to the major flare but a great deal of activity in the filament that separated the opposite magnetic polarities of the active region. Large proper motions of sunspots and magnetic fields suggest that the magnetic field was stressed prior to the flare. The immediate trigger of the flare appears to have been an eruption of new magnetic flux in the center of the active region. The new flux erupted in a configuration that decreased the net flux of the active region and contributed to the decay of the region. 相似文献
129.
Livingstone C.E. Gray A.L. Hawkins R.K. Olsen R.B. 《Aerospace and Electronic Systems Magazine, IEEE》1988,3(10):11-20
The airborne synthetic-aperture radar (SAR) system developed for the Canada Centre for Remote Sensing (CCRS) is described. It consists of two radars, at C -band and X -band. Each radar incorporates the following features: dual-channel receivers and dual-polarized antennas; a high quality, 7-look, real-time processor; a sensitivity time control for range-dependent gain control; a motion-compensation system for antenna steering in azimuth and elevation; and baseband I and Q signal phase rotation. The system also uses a high-power transmitter with a low-power back-up. The SAR maps to either side of the aircraft, at high or low resolution, at incidence angles which in high resolution span 0° to 80°. Radar operating parameters, data products, key specifications and the motion compensation scheme used are presented. Properties of the real-time imagery are discussed and examples of C -band SAR data in the three operating modes are given 相似文献
130.