全文获取类型
收费全文 | 3478篇 |
免费 | 2篇 |
国内免费 | 6篇 |
专业分类
航空 | 1808篇 |
航天技术 | 991篇 |
综合类 | 5篇 |
航天 | 682篇 |
出版年
2021年 | 13篇 |
2019年 | 14篇 |
2018年 | 171篇 |
2017年 | 146篇 |
2016年 | 58篇 |
2015年 | 36篇 |
2014年 | 50篇 |
2013年 | 61篇 |
2012年 | 88篇 |
2011年 | 207篇 |
2010年 | 184篇 |
2009年 | 227篇 |
2008年 | 236篇 |
2007年 | 193篇 |
2006年 | 47篇 |
2005年 | 113篇 |
2004年 | 84篇 |
2003年 | 91篇 |
2002年 | 46篇 |
2001年 | 104篇 |
2000年 | 45篇 |
1999年 | 86篇 |
1998年 | 85篇 |
1997年 | 62篇 |
1996年 | 63篇 |
1995年 | 88篇 |
1994年 | 97篇 |
1993年 | 42篇 |
1992年 | 61篇 |
1991年 | 22篇 |
1990年 | 28篇 |
1989年 | 56篇 |
1988年 | 20篇 |
1987年 | 35篇 |
1986年 | 19篇 |
1985年 | 74篇 |
1984年 | 42篇 |
1983年 | 46篇 |
1982年 | 55篇 |
1981年 | 77篇 |
1980年 | 26篇 |
1979年 | 24篇 |
1978年 | 22篇 |
1977年 | 18篇 |
1976年 | 15篇 |
1975年 | 18篇 |
1974年 | 12篇 |
1972年 | 17篇 |
1969年 | 13篇 |
1966年 | 8篇 |
排序方式: 共有3486条查询结果,搜索用时 15 毫秒
961.
962.
963.
964.
Transfers with a low thrust are considered under constraints imposed on the thrust vector direction. These constraints can be caused by peculiarities of the attitude control system and the mode of stabilization of a spacecraft, and, in the general case, they are functions of the time and state vector. The constraints specified by equalities and inequalities are investigated. It is shown that the optimal thrust is directed along the projection of the Lawden’s primer vector onto the restricting set. 相似文献
965.
A novel guidance law designed specifically for a missile having forward and aft control systems is presented. For the derivation a linear quadratic differential games formulation of the end-game interception scenario is used. Conditions for achieving perfect intercept are given and new game spaces are presented. It is also shown that increasing the direct lift associated with the canard control allows intercepting targets with higher maneuvering capability, while for the tail control the effect is opposite. 相似文献
966.
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
967.
N. N. Inozemtsev 《Russian Aeronautics (Iz VUZ)》2010,53(4):443-449
A problem of applying closed multiloop thermodynamic cycles with mixing of dissimilar working gases in spacecraft power plants
has been considered. The advantage of these cycles that is due to reduction of a heat quantity being rejected into space has
been shown for ecologically clean generation of electric energy in prolonged space flights. 相似文献
968.
The mathematical models of the solid-liquid flow regimes in the vertical cylindrical channel are described. A two-speed flow
based on the solid-liquid phase interaction is considered. The problem was numerically solved and the calculation results
were compared with experimental data. 相似文献
969.
A procedure of calculating an axial radial-flow centrifugal stage is considered. Using the gas-dynamically expedient load
ratio distribution in profile, the process of impeller flow passage profiling is described. Also given are some techniques
for decreasing or eliminating a wake zone as well as a graph of loss dependence on the divergence factor and velocity deceleration
on the rarefaction side of the blade channel at the impeller outlet. 相似文献
970.
A comprehensive numerical study of transient interchamber processes occurring when reaching the SPRE operational conditions
is carried out. A conjugate problem under consideration includes nonstationary operation of an igniter heating, ignition and
subsequent nonstationary and turbulent burning of a solid-propellant charge; nonstationary three-phase homo-heterogeneous
flow of combustion products in the combustion chamber, nozzle and downstream of the nozzle block of a rocket engine; motion
of a nozzle block cover. The calculation results are presented. 相似文献