全文获取类型
收费全文 | 919篇 |
免费 | 243篇 |
国内免费 | 146篇 |
专业分类
航空 | 898篇 |
航天技术 | 147篇 |
综合类 | 113篇 |
航天 | 150篇 |
出版年
2024年 | 4篇 |
2023年 | 10篇 |
2022年 | 40篇 |
2021年 | 39篇 |
2020年 | 57篇 |
2019年 | 54篇 |
2018年 | 52篇 |
2017年 | 55篇 |
2016年 | 43篇 |
2015年 | 57篇 |
2014年 | 77篇 |
2013年 | 59篇 |
2012年 | 74篇 |
2011年 | 85篇 |
2010年 | 85篇 |
2009年 | 72篇 |
2008年 | 59篇 |
2007年 | 62篇 |
2006年 | 51篇 |
2005年 | 40篇 |
2004年 | 37篇 |
2003年 | 29篇 |
2002年 | 20篇 |
2001年 | 20篇 |
2000年 | 15篇 |
1999年 | 16篇 |
1998年 | 16篇 |
1997年 | 9篇 |
1996年 | 12篇 |
1995年 | 9篇 |
1994年 | 5篇 |
1993年 | 8篇 |
1992年 | 9篇 |
1991年 | 10篇 |
1990年 | 9篇 |
1989年 | 4篇 |
1988年 | 2篇 |
1987年 | 3篇 |
排序方式: 共有1308条查询结果,搜索用时 781 毫秒
831.
导弹飞行试验时制导系统误差系数(工具误差)与地面试验的误差系数是否一致(或部分一致),这是人们比较关心的问题,本文从理论上介绍了线性模型假设检验方法,应用这种方法检验制导系统工具误差天地因子的一致性,若一致(或部分一致)则验前信息可被充分利用以提高制导系统误差系数分离的效果。 相似文献
832.
本文介绍一种快速线网提取方法,该算法是采用图论中求无向图连通分量的方法实现的,取得较好的结果。 相似文献
833.
834.
大型双曲冷却塔平均风荷载的数值模拟研究 总被引:3,自引:0,他引:3
对双曲冷却塔的平均风荷载进行CFD数值模拟,获得冷却塔内外表面的三维流场特性和各高度截面的平均风压系数分布曲线,并与以往文献的实测数据和风洞试验结果进行比较,以验证数值模拟的准确性.根据内外表面的风速矢量图,描述冷却塔内外流体的流动特征,发现旋涡的存在使风压分布趋于均匀的规律.并分析塔底的边缘效应及其对冷却塔内外表面风压的影响.讨论现行设计规范在外压的三维效应和内外压的共同作用等方面的不完善之处,给出部分改进建议和冷却塔外表面、内表面和内外表面压差的风压系数等压图,以供设计参考. 相似文献
835.
836.
本文通过对摩擦系数f=0.1~0.2范围内9个f档级M12-M48范围中12种尺寸的标准粗牙螺栓,共12种情况下K值的具体计算及综合分析,给出了K值与摩擦系数间的简单关系。 相似文献
837.
838.
N. Pierdicca C. Bignami M. Roca P. Féménias M. Fascetti M. Mazzetta C.N. Loddo A. Martini S. Pinori 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
Although the history of spaceborne altimeters goes back to the early seventies, the absolute calibration of the backscattering coefficient has never been deeply investigated. This information has been primarily used to infer the wind speed via an empirical model, and the intercalibration among different satellite altimeters has revealed to be suitable for this purpose, being the wind retrieval based on an empirical relationship. As far as Ku band system is concerned, the sigma naught absolute calibration of the Envisat altimeter (RA-2) has been performed using an active reference target provided by a transponder. This has been exploited during the 6-month Commissioning phase to generate early calibration results. In order to monitor the RA-2 backscatter calibration during the Envisat lifetime, a continuous calibration effort has been carried out by operating the transponder as much as possible. This paper aims to review the entire effort for calibrating the RA-2 sigma naught measurements, which lasted for almost seven years. It presents in detail the adopted methodology and the final outcome of the activity, providing the users with the correction (bias) to get the calibrated sigma naught and analyzing its stability during almost the entire Envisat lifetime. Specifically, it is concluded that the RA-2 backscatter measurements were quite stable, even if a bias of about 1 dB should be considered with respect to the actually released product. Some small changes in the bias as function of time can be identified during most of the Envisat lifetime, consisting in a slight increase in the first two years, followed by a more stable period and a final drop observed at the end of 2009, until the conclusion of the calibration activity (corresponding to the change in Envisat orbit). 相似文献
839.
R. Jehn V. Companys C. Corral D. Garca Yrnoz N. Snchez 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,42(8):1364-1369
BepiColombo is scheduled for launch in August 2013 and to arrive after a nearly six-year long transfer at Mercury in June 2019. The trajectory has a number of challenging elements: a launch with Soyuz/Fregat into a geostationary transfer orbit, followed by a lunar flyby, long low-thrust arcs and five more planetary flybys (one at the Earth, two at Venus and two at Mercury). At arrival the low thrust arcs reduce the approach velocity so much that BepiColombo passes by the Sun–Mercury Lagrange points L1 and L2 and gets weakly captured in a highly eccentric orbit around Mercury in case the orbit insertion manoeuvre would fail.This paper describes the navigation strategy during the final phase. Five trajectory correction manouevres during the last 65 days requiring up to 20 m/s (3σ) are proposed. With this strategy it is possible to navigate BepiColombo safely through the weak-stability boundary of Mercury and to reach the target periherm with a precision of 11 km. 相似文献
840.
蔡靖 《中国民航学院学报》2008,26(6):32-36
为了更好地解决基桩缺陷量化分析问题,从建立成层土中缺陷桩桩土系统模型入手,引入矩阵递推法,求解出成层土中多缺陷桩桩顶和桩身任意点的瞬态响应解析解,并应用此解对缺陷桩瞬态响应影响参数进行分析,得出在利用幅值比进行缺陷量化分析方法中的关键影响因素为桩侧土阻尼系数,为成层土中基桩缺陷量化分析和承载力评价奠定了理论基础。 相似文献