全文获取类型
收费全文 | 4551篇 |
免费 | 679篇 |
国内免费 | 1000篇 |
专业分类
航空 | 2621篇 |
航天技术 | 1363篇 |
综合类 | 830篇 |
航天 | 1416篇 |
出版年
2024年 | 9篇 |
2023年 | 11篇 |
2022年 | 49篇 |
2021年 | 60篇 |
2020年 | 117篇 |
2019年 | 37篇 |
2018年 | 44篇 |
2017年 | 41篇 |
2016年 | 74篇 |
2015年 | 146篇 |
2014年 | 289篇 |
2013年 | 283篇 |
2012年 | 301篇 |
2011年 | 315篇 |
2010年 | 454篇 |
2009年 | 350篇 |
2008年 | 353篇 |
2007年 | 322篇 |
2006年 | 252篇 |
2005年 | 218篇 |
2004年 | 144篇 |
2003年 | 146篇 |
2002年 | 120篇 |
2001年 | 198篇 |
2000年 | 196篇 |
1999年 | 239篇 |
1998年 | 225篇 |
1997年 | 182篇 |
1996年 | 169篇 |
1995年 | 128篇 |
1994年 | 109篇 |
1993年 | 128篇 |
1992年 | 98篇 |
1991年 | 101篇 |
1990年 | 79篇 |
1989年 | 81篇 |
1988年 | 54篇 |
1987年 | 37篇 |
1986年 | 21篇 |
1985年 | 12篇 |
1984年 | 5篇 |
1983年 | 13篇 |
1982年 | 9篇 |
1981年 | 6篇 |
1975年 | 2篇 |
1974年 | 1篇 |
1969年 | 1篇 |
1900年 | 1篇 |
排序方式: 共有6230条查询结果,搜索用时 11 毫秒
321.
A simple and fast zero tracking algorithm for adaptive arrays with large look direction errors is presented and investigated. Basically, the algorithm is based on adjusting the complex zeroes of a power inversion array in a time-multiplexed manner to track all the sources in the environment. To preserve the desired signal which is supposed to be closest to the look direction of 0°, the algorithm removes the zero with the shortest distance to ej0 so that the directional response consists of only nulls steered at the jammers. When compared with the least mean square (LMS) algorithm employing zeroth and first-order look direction constraints, the new algorithm has about the same implementation complexity, is considerably faster, and possesses a much better signal-to-noise ratio (SNR) performance when the look direction is erroneous 相似文献
322.
This study presents a methodology for specifying a neural controller for a system about which no a priori model information is available. The neural design presumes that a finite duration input/output (I/O) histogram on the system is available. The design procedure extracts from the histogram sufficient information to specify the neural feedback controller. The resultant controller will drive the system along a general output reference profile (unknown during the design). The resultant controller also exhibits the capability of disturbance rejection and the capacity to stabilize unstable plants 相似文献
323.
刘山 《中国民航学院学报》1995,13(1):40-44
本文通过一个应用系统的编制过程,阐述了用数据库技术实现超文本多媒体技术的方法。 相似文献
324.
325.
326.
327.
328.
利用实时遥测飞行信息生成三维虚拟地形场景,旨在飞机试飞时,增强地面指挥人员对飞机实时位置地面场景的感知能力,帮助飞行员在试飞时处理复杂多变的飞行状况。为了逼真且流畅地生成三维地形场景,首先使用固定网格映射(PGM)的方法生成地形采样网格,接着利用几何着色器为三角形面片分配连续的与视点相关的细节等级(LOD),对缓存在纹理数组中的各等级高程数据和卫星照片进行混合采样。由于细节等级是连续的,因此各级纹理和高程之间能够平滑的过渡,增加了场景的真实性。最后,考虑到显存的容量限制,引入了一种内存与显存之间的纹理调度方法。整个算法都是面向图形处理单元(GPU)实现的,能够较好地兼顾实时性和真实性,实现多分辨率大规模地形场景的实时虚拟显示。根据本文算法实现的实时监控系统在支线飞机的飞行试验中取得了较好的效果。 相似文献
329.
Oxygen plasma source generated by thermal cathode filament discharge has been used to study the erosion process of polyimide (PI) materials in atomic oxygen (AO) environment, and their mass loss, surface morphology and surface chemical compositions have been examined by scanning electron microscope (SEM) and X-ray photoelectron spectroscopy (XPS) after exposure to incremental AO flux. The data indicate that the physical adsorption of AO at the samples' surface results in the increase of oxygen concentration when polyimide is exposed to AO flux. Then selective chemical reactions of groups of polyimide materials with AO yield volatile organic compounds, sample mass loss is on linear increase and carpet-like surface morphology forms. In the initial exposure to AO, the reaction occurs mainly between AO and carbon in specific location of aromatic ring, then the reaction rate of C=O groups gradually increases. After AO exposure, the oxygen concentration increases while nitrogen and carbon concentration decreases. Reaction rate of groups containing nitrogen is slower compared with carbon and oxygen. 相似文献
330.
Multi-frequency RCS Reduction Characteristics of Shape Stealth with MLFMA with Improved MMN 总被引:6,自引:0,他引:6
Three new control factors are presented for calculating the multipole mode number (MMN) efficiently and precisely. The effects of these control factors on the number of integral samples and the precision of multilevel fast multipole algorithm (MLFMA) are investigated. A new approach based on control factors which is proven to be able to improve the computational efficiency and reduce the needed memory significantly as well as ensuring the proper precision. For three aircraft models, the improved MLFMA is employed to analyze their multi-frequency scattering characteristics. It is found that aircraft shape can influence radar cross section (RCS) in different frequency zones. Both the multi-frequency RCS reduction characteristics of shape stealth aircraft and the conventional aircraft with stealth design taken into account are investigated, and the results show that shape stealth exhibits significant RCS reduction in the resonance and high-frequency zones, and with a weaker influence in the Rayleigh zone. Compared with radar absorbing material (RAM), shape stealth yields a wider multi-frequency RCS reduction. The above-mentioned results can be applied to stealth design for multiple frequencies or even for all frequencies. 相似文献