全文获取类型
收费全文 | 602篇 |
免费 | 84篇 |
国内免费 | 123篇 |
专业分类
航空 | 399篇 |
航天技术 | 234篇 |
综合类 | 75篇 |
航天 | 101篇 |
出版年
2024年 | 1篇 |
2023年 | 4篇 |
2022年 | 11篇 |
2021年 | 16篇 |
2020年 | 25篇 |
2019年 | 32篇 |
2018年 | 57篇 |
2017年 | 39篇 |
2016年 | 27篇 |
2015年 | 20篇 |
2014年 | 32篇 |
2013年 | 24篇 |
2012年 | 33篇 |
2011年 | 34篇 |
2010年 | 35篇 |
2009年 | 50篇 |
2008年 | 49篇 |
2007年 | 37篇 |
2006年 | 52篇 |
2005年 | 40篇 |
2004年 | 24篇 |
2003年 | 31篇 |
2002年 | 11篇 |
2001年 | 7篇 |
2000年 | 15篇 |
1999年 | 10篇 |
1998年 | 11篇 |
1997年 | 11篇 |
1996年 | 10篇 |
1995年 | 11篇 |
1994年 | 20篇 |
1993年 | 9篇 |
1992年 | 6篇 |
1991年 | 4篇 |
1990年 | 6篇 |
1989年 | 3篇 |
1984年 | 2篇 |
排序方式: 共有809条查询结果,搜索用时 101 毫秒
351.
Shiqiang Zheng Bangcheng Han 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
This paper presents an integrated angular velocity measurement and attitude control system of spacecraft using magnetically suspended double-gimbal control moment gyros (MSDGCMGs). The high speed rotor of MSDGCMG is alleviated by a five-degree-of-freedom permanent magnet biased AMB control system. With this special rotor supported manner, the MSDGCMG has the function of attitude rate sensing as well as attitude control. This characteristic provides a new approach to a compact light-weight spacecraft design, which can combine these two functions into a single device. This paper discusses the principles and implementations of AMB-based angular velocity measurement. Spacecraft dynamics with DGMSCMG actuators, including the dynamics of magnetically suspended high-speed rotor, the dynamics of inner gimbal and outer gimbal, as well as the determination method of spacecraft angular velocity are modeled, respectively. The effectiveness of the proposed integrated system is also validated numerically and experimentally. 相似文献
352.
M.T. Menna A. Papitto L. Burderi T. Di Salvo F. DAntona N.R. Robba 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2006,38(12):2704-2706
We analyze the three outbursts of the X-ray millisecond pulsar SAX J1808.4-3658 that occurred in 1998, 2000, and 2002 observed with RXTE. With a technique based on epoch folding search we find an unique orbital solution valid over the five years of high temporal resolution data available. We revise the estimate of the orbital period, Porb = 7249.1569(1) s and of its error, which we decrease by one order of magnitude. We also give the first constraint on the orbital period derivative, . We find that in 2002 the pulse profile shape is clearly asymmetric, showing a secondary peak at about 145° from the main pulse, which is different from the sinusoidal shape reported at the beginning of the 1998 outburst. 相似文献
353.
The surface wave induced magnetic reconnection (SWIMR) model based on Alfven Resonance theory will be discussed briefly both
for collisional and collisionless plasmas. It is shown that the spatial scales and time delays associated with Flux Transfer
Events and Pulsed Ionospheric Flows, as observed by satellites and SuperDARN radars and the magnetic bubbles, observed at
the high latitude boundary of the magnetopause, can be explained by the SWIMR model.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
354.
Steven R. Spangler 《Space Science Reviews》2005,121(1-4):189-200
I discuss a method for determining the strength and spatial structure of the coronal magnetic field by observations of the
Faraday rotation of a radio galaxy which is in conjunction with the Sun. Given a knowledge of the plasma density in the outer
corona, and the magnetic field sector structure (both independently available), the strength of the coronal field can be determined,
as well as the magnitude of spatial variations on scales of 1000 km to several solar radii. Such knowledge is crucial for
testing computational models of the solar corona, which are prominently featured in this meeting. Results are presented from
observations with the Very Large Array radio telescope of the radio galaxy 3C228 on August 16, 2003, when the line of sight
to the source was at heliocentic distances of 7.1−6.2R
⊙. The observations are consistent with a coronal magnetic field which is proportional to the inverse square of the distance
in the range 6 ≤ r ≤ 10R
⊙, and has a value of 39 mG at 6.2R
⊙. The Faraday rotation is uniform across the source, indicating an absence of strong plasma inhomogeneity on spatial scales
up to 35,000 km. 相似文献
355.
356.
357.
环形磁铁空间磁场的解析计算与仿真 总被引:1,自引:0,他引:1
从永磁体的磁荷模型出发,运用标量磁位法、广义二项式定理、矢量叠加原理等建立了环形磁铁在磁体外部空间磁场分布的解析表达式,并在MATLAB仿真软件中进行了计算。利用三维数字式特斯拉计实际测量了两种规格的永磁体的磁场分布,利用Ansoft Maxwell电磁场分析软件建立了两种永磁体在磁体外部空间的磁场分布,通过对比解析计算结果、实际测量结果和Ansoft Maxwell仿真结果发现解析表达式很好地反映了永磁环空间磁场的分布规律,误差不超过7%,从而验证了解析表达式的正确性。 相似文献
358.
介绍了从俄罗斯引进的用于交变磁场的国防标准——交变中磁标准装置的基本工作原理,以及对其设计方案的剖析。该标准装置工作频率(20~1 000)Hz,复现交变磁场强度(0.1~1 000)mT,在这一领域内代表国际最高水平。通过对其信号获取、磁场感应信号的放大处理、大电流的产生办法、安全互锁设计,以及整体系统理论计算的分析,为该领域内标准装置的国产化提供理论基础,具有较好的实用价值。 相似文献
359.
360.
以开环不稳定和强烈非线性的磁悬浮转台为研究对象,其控制器性能的好坏直接影响到磁悬浮转台的动态性能。模糊控制因其简单实用,不需要精确的数学模型等特点而成为磁悬浮控制系统的理想选择。采用模糊控制方法实现对磁悬浮转台的数字控制,利用M atlab模糊逻辑工具箱中的FIS(Fuzzy Inference System)编辑器,结合S imu link工具箱建立了模糊控制系统的仿真模型,并对整个系统进行了仿真和实验。仿真结果表明模糊控制器在磁悬浮转台起动和悬浮时响应速度快,稳定性好,抗干扰能力强。 相似文献