全文获取类型
收费全文 | 7861篇 |
免费 | 16篇 |
国内免费 | 19篇 |
专业分类
航空 | 3772篇 |
航天技术 | 2587篇 |
综合类 | 23篇 |
航天 | 1514篇 |
出版年
2021年 | 61篇 |
2018年 | 223篇 |
2017年 | 168篇 |
2016年 | 121篇 |
2015年 | 63篇 |
2014年 | 175篇 |
2013年 | 211篇 |
2012年 | 227篇 |
2011年 | 371篇 |
2010年 | 276篇 |
2009年 | 402篇 |
2008年 | 459篇 |
2007年 | 281篇 |
2006年 | 169篇 |
2005年 | 247篇 |
2004年 | 206篇 |
2003年 | 240篇 |
2002年 | 141篇 |
2001年 | 244篇 |
2000年 | 114篇 |
1999年 | 159篇 |
1998年 | 191篇 |
1997年 | 139篇 |
1996年 | 148篇 |
1995年 | 209篇 |
1994年 | 216篇 |
1993年 | 119篇 |
1992年 | 148篇 |
1991年 | 78篇 |
1990年 | 72篇 |
1989年 | 138篇 |
1988年 | 66篇 |
1987年 | 65篇 |
1986年 | 72篇 |
1985年 | 192篇 |
1984年 | 179篇 |
1983年 | 149篇 |
1982年 | 148篇 |
1981年 | 239篇 |
1980年 | 68篇 |
1979年 | 63篇 |
1978年 | 63篇 |
1977年 | 52篇 |
1976年 | 54篇 |
1975年 | 53篇 |
1974年 | 50篇 |
1973年 | 49篇 |
1972年 | 59篇 |
1971年 | 40篇 |
1970年 | 40篇 |
排序方式: 共有7896条查询结果,搜索用时 46 毫秒
931.
V. G. Fainshtein 《Cosmic Research》2007,45(5):384-392
A positive correlation is shown to exist between the angular sizes (in the sky plane) of eruptive prominences and/or post-eruptive arcades and coronal mass ejections (CMEs) associated with them. New regularities are found that characterize the relationship between the latitude of eruptive prominences (post-eruptive arcades) and the latitude position of CMEs associated with them in the field of view of a coronagraph. An interpretation of these regularities is given. 相似文献
932.
933.
Lobanov V.S. Tarasenko N.V. Shulga D.N. Zboroshenko V.N. Fedotov V.P. 《Aerospace and Electronic Systems Magazine, IEEE》2007,22(4):23-29
In article the opportunity of use strapdown inertial navigation system (SINS) on the base of fiber-optic gyroscopes and quartz accelerometers corrected from star sensors and satellite navigation equipment (SNE) for perspective interplanetary spacecrafts motion control on phases of interplanetary trajectory insertion, trajectory correction, and braking during transition to Mars orbit is investigated. Results of onboard control complex accuracy characteristics estimation are presented at the given dynamic spacecraft scheme which is taking into account the liquid oscillations in tanks and structure elements elasticity. At modelling the errors of measuring devices installation, errors of SINS initial alignment and instrumental errors of SINS sensitive elements, variation of control engines parameters were taken into account. The structure of the developed complex of imitation modelling of interplanetary spacecraft controlled motion is resulted. Estimations of active flight legs realization accuracy were received by a method of statistical modelling of spacecraft controlled motion 相似文献
934.
935.
A numerical investigation of the melt flow and heat and mass transfer is carried out at the crystal growth under zero gravity, when the melt detachment from ampoule walls, crystal vibration, and various magnetic fields are active. Specific features of the melt flow are demonstrated depending on the size of a detachment zone adjacent to the crystallization boundary. The velocity of the averaged flow generated by crystal vibration is determined as a function of the vibration intensity. It is shown that the crystal vibration cannot compensate a thermal capillary flow (caused by detachment of the melt from the ampoule wall) and reduce the macrosegregation of impurities. It is shown that the application of steady and rotating magnetic fields are inefficient for all ampoule methods of crystal growth under microgravity conditions. 相似文献
936.
McEneaney W.M. Fitzpatrick B.G. Lauko I.G. 《IEEE transactions on aerospace and electronic systems》2004,40(4):1191-1216
A command and control (C/sup 2/) problem for military air operations is addressed. Specifically, we consider C/sup 2/ problems for air vehicles against ground-based targets and defensive systems. The problem is viewed as a stochastic game. We restrict our attention to the C/sup 2/ level where the problem may consist of a few unmanned combat air vehicles (UCAVs) or aircraft (or possibly teams of vehicles), less than say, a half-dozen enemy surface-to-air missile air defense units (SAMs), a few enemy assets (viewed as targets from our standpoint), and some enemy decoys (assumed to mimic SAM radar signatures). At this low level, some targets are mapped out and possible SAM sites that are unavoidably part of the situation are known. One may then employ a discrete stochastic game problem formulation to determine which of these SAMs should optimally be engaged (if any), and by what series of air vehicle operations. We provide analysis, numerical implementation, and simulation for full state-feedback and measurement feedback control within this C/sup 2/ context. Sensitivity to parameter uncertainty is discussed. Some insight into the structure of optimal and near-optimal strategies for C/sup 2/ is obtained. The analysis is extended to the case of observations which may be affected by adversarial inputs. A heuristic based on risk-sensitive control is applied, and it is found that this produces improved results over more standard approaches. 相似文献
937.
938.
L. G. Blomberg J. A. Cumnock 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2004,33(12):2161-2165
Mercury has a small but intriguing magnetosphere. In this brief review, we discuss some similarities and differences between Mercury’s and Earth’s magnetospheres. In particular, we discuss how electric and magnetic field measurements can be used as a diagnostic tool to improve our understanding of the dynamics of Mercury’s magnetosphere. These points are of interest to the upcoming ESA-JAXA BepiColombo mission to Mercury. 相似文献
939.
We describe a numerical integral-projection method used by the authors for the approximate solution of systems of interrelated two-dimensional linear boundary-value problems in mechanics of composite shell systems. The method is based on discretization in each shell substructure of a two-dimensional problem along one of coordinates using a projection-grid variant of the Galerkin-Petrov method and its subsequent transformation to a system of ordinary differential equations; by integration and introduction of sought functions as unknown derivatives, the system is reduced to a system of integral equations being solved by the method of mechanical quadratures. The method is characterized by the fact that its application requires no additional conditions of conformity with discretization parameters of substructures being mated. 相似文献
940.
R. Musci T. SchildknechtT. Flohrer G. Beutler 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(7):1071-1076
A new population of uncatalogued objects in geosynchronous Earth orbits (GEO), with a mean motion of about 1 rev/day and eccentricities up to 0.6, has been identified recently. The first observations of this new type of objects were acquired in the framework of the European Space Agency’s (ESA) search for space debris in GEO and the geostationary transfer orbit (GTO) using the ESA 1-m telescope on Tenerife. Earlier studies have postulated that the perturbations due to the solar radiation pressure can lead to such large eccentricities for GEO objects with a high area-to-mass ratio (A/M). The simulations showed that the eccentricities of GEO objects with large A/M exhibit periodic variations with periods of about one year and amplitudes depending on the value of A/M. The findings of these studies could be confirmed by observations from the ESA 1-m telescope on Tenerife. 相似文献