全文获取类型
收费全文 | 10336篇 |
免费 | 9357篇 |
国内免费 | 1768篇 |
专业分类
航空 | 17835篇 |
航天技术 | 1354篇 |
综合类 | 385篇 |
航天 | 1887篇 |
出版年
2024年 | 102篇 |
2023年 | 197篇 |
2022年 | 296篇 |
2021年 | 347篇 |
2020年 | 463篇 |
2019年 | 1152篇 |
2018年 | 1332篇 |
2017年 | 1256篇 |
2016年 | 1291篇 |
2015年 | 1227篇 |
2014年 | 1102篇 |
2013年 | 1093篇 |
2012年 | 1053篇 |
2011年 | 954篇 |
2010年 | 997篇 |
2009年 | 1026篇 |
2008年 | 893篇 |
2007年 | 749篇 |
2006年 | 576篇 |
2005年 | 390篇 |
2004年 | 379篇 |
2003年 | 345篇 |
2002年 | 373篇 |
2001年 | 315篇 |
2000年 | 291篇 |
1999年 | 335篇 |
1998年 | 309篇 |
1997年 | 258篇 |
1996年 | 222篇 |
1995年 | 203篇 |
1994年 | 193篇 |
1993年 | 247篇 |
1992年 | 170篇 |
1991年 | 342篇 |
1990年 | 291篇 |
1989年 | 312篇 |
1988年 | 220篇 |
1987年 | 91篇 |
1986年 | 38篇 |
1985年 | 4篇 |
1984年 | 4篇 |
1983年 | 8篇 |
1982年 | 3篇 |
1981年 | 7篇 |
1979年 | 1篇 |
1972年 | 1篇 |
1965年 | 2篇 |
1962年 | 1篇 |
排序方式: 共有10000条查询结果,搜索用时 15 毫秒
11.
12.
T. J. Ponman A. M. Read 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1993,13(12):361-364
Using data from the Wide Field Camera EUV all-sky survey, we have established upper limits to the EUV flux from a sample of 30 bright, nearby, non-active spiral galaxies. These galaxies were chosen to be those most likely to be detected in the EUV on the basis of (i) low interstellar absorption within our own galaxy, (ii) brightness in other wavebands, (iii) high star formation activity, and (iv) proximity. The derived EUV upper limits are restrictive, and establish for the first time that the EUV flux escaping from galaxies does not constitute a major component of their bolometric luminosity, and in particular that it cannot be the sink for the energy injected into the interstellar medium by supernova explosions, as had been suggested following the failure to detect this power in the X-ray band. 相似文献
13.
The authors present a new scientific space mission consisting of a satellite carrying a receiving- only SAR which receives the signal transmitted by the ENVISAT-1 SAR. The integration of ENVISAT-1 SAR and bistatic radar data offers an improved potentiality of surface classification, three-dimensional observation, and the opportunity of advanced scientific experiments in the field of bistatic scattering. The small satellite nominal orbit and the attitude manoeuvres are designed in order to maintain an adequate overlap between the two radar swaths along the whole orbit, taking into account the ENVISAT-1 attitude and pointing. A preliminary satellite design (2-year lifetime) is then performed to evaluate the orbit decay and to determine the appropriate orbit manoeuvres (every 4 days) to control the satellites relative phase. The numerical simulation shows that a spacecraft of about 584kg is able to meet the mission requirements. 相似文献
14.
In extension to common applications such as groundtrack displays and antenna steering, the SGP4 orbit model is proposed for operational orbit determination in small satellite missions. SGP4 is an analytical orbit model for Low-Earth orbiting satellites that is widely used for the propagation of NORAD twoline elements. Twoline elements may hence be generated completely independent of NORAD. Their use as exclusive source of orbital information simplifies the operations concept and reduces mission costs through the extensive use of existing low-cost mission support software. Due to small computer resource requirements of 8–10kByte, the SGP4 model may also be applied for onboard orbit computations making use of e.g. a 80186 processor, thus ensuring full compatibility of ground-based and onboard operations. The proposed approach is particularly suited in combination with a space-borne GPS receiver, were the C/A-code navigation solutions are treated as measurements that are adjusted in a least-squares sense using the SGP4 model. As consequence, inherent drawbacks of the pure navigation solutions such as data gaps and scatter as well as limited velocity accuracy are avoided, while the operational navigation activities are kept at a minimum. The feasibility of the concept is illustrated based on real GPS navigation data from the TOPEX/Poseidon and the MIR space station with an inherent data quality of 50–100 m. It is shown that 3 hours of data within a 4 day period are sufficient to keep the position error within 4 km, that is considered sufficient for most applications. 相似文献
15.
16.
摩擦塞焊研发与关键问题 总被引:1,自引:0,他引:1
如果将搅拌摩擦焊认定为铝合金焊接上的一场革命,摩擦塞焊则是铝合金补焊工艺上一次质的飞跃。文章阐明了摩擦塞焊的工作原理,详细论述该工艺的发展、研发中出现的几个关键问题和解决途径。 相似文献
17.
Tsai-Fu Wu Chh-Lung Shen Chien-Hsuan Chang Jeiyang Chiu 《IEEE transactions on aerospace and electronic systems》2003,39(2):635-646
This paper presents a single-phase three-wire (1/spl phi/ 3W) grid-connection photovoltaic (PV) power inverter with a of partial active power filter (PAPF) feature, which can not only deal with PV power but filter current harmonics and improve power factor. Once the processed power exceeds the switch ratings, the inverter can reduce its output reactive power and harmonic power, while still supplying the maximum real power generated by the PV arrays. In the derivation of control laws, a limit circle is defined to confine the output power of the inverter. To determine the power that the inverter can process, the instantaneous reactive power of a 1/spl phi/ 3W system is defined and used to calculate reactive power, which can avoid complex detections of phase angle and magnitude of the fundamental component of a nonlinear load current. Simulation results and experimental measurements have verified the proposed algorithm and the feasibility of the inverter. 相似文献
18.
数据采集系统的总体评价 总被引:5,自引:0,他引:5
从性能指标出发,综述了数据采集系统总结评价技术的发展状况。并提出了对数据采集系统性能指标的两类分类方法 。 相似文献
19.
多重直扩信号的快速捕获 总被引:1,自引:0,他引:1
多重直扩信号的快速捕获得卫星定位及通信系统研制过程中遇到的一个主要课题,它的实现,不仅可以提高系统的多址能力,而且也是系统实现的必备条件,本文阐明了多重直扩信号的来源以及可被分离的理论依据,给出了多重直扩信号快速捕获的硬件实现方案及部分实验结果,得出了一些重要结论。 相似文献
20.
数字地形数据的二维三次卷积插值 总被引:6,自引:3,他引:6
由于数字地形数据库是以网格的形式给出网格点上的地形高度信息,在低空突防轨迹优化过程中,往往需要非网格蹼地形的高度信息和地形曲面的导数,这些都是离散的地形数据库所无法提供的。对二维的地形数据进行插值是解决问题的有效手段。本文提出一种二维离散数据的插值方法--二维三次卷积插值。该插值函数是地形曲面的三次逼近,具有连续的三阶导数,可以非常好地满足低空突防轨迹优化的需要。仿真结果表明,它具有比双线性插值和 相似文献