全文获取类型
收费全文 | 4696篇 |
免费 | 740篇 |
国内免费 | 970篇 |
专业分类
航空 | 2738篇 |
航天技术 | 1302篇 |
综合类 | 860篇 |
航天 | 1506篇 |
出版年
2024年 | 6篇 |
2023年 | 20篇 |
2022年 | 61篇 |
2021年 | 74篇 |
2020年 | 125篇 |
2019年 | 44篇 |
2018年 | 60篇 |
2017年 | 61篇 |
2016年 | 92篇 |
2015年 | 147篇 |
2014年 | 290篇 |
2013年 | 276篇 |
2012年 | 320篇 |
2011年 | 326篇 |
2010年 | 446篇 |
2009年 | 368篇 |
2008年 | 365篇 |
2007年 | 353篇 |
2006年 | 268篇 |
2005年 | 235篇 |
2004年 | 150篇 |
2003年 | 156篇 |
2002年 | 115篇 |
2001年 | 204篇 |
2000年 | 196篇 |
1999年 | 230篇 |
1998年 | 217篇 |
1997年 | 177篇 |
1996年 | 172篇 |
1995年 | 129篇 |
1994年 | 120篇 |
1993年 | 127篇 |
1992年 | 99篇 |
1991年 | 97篇 |
1990年 | 71篇 |
1989年 | 79篇 |
1988年 | 50篇 |
1987年 | 31篇 |
1986年 | 16篇 |
1985年 | 9篇 |
1984年 | 3篇 |
1983年 | 4篇 |
1982年 | 7篇 |
1981年 | 5篇 |
1975年 | 2篇 |
1974年 | 1篇 |
1969年 | 1篇 |
1900年 | 1篇 |
排序方式: 共有6406条查询结果,搜索用时 15 毫秒
1.
仅测角自主导航方法具有设备简单、复杂度低,功耗低的优点,在空间任务中具有广泛的应用前景.针对中远距离下空间目标特征少的特点,提出了一种利用基于OPTICS聚类算法的空间目标检测方法,可用于仅测角导航过程中的目标检测.对原始星图进行预处理提取星点及目标点,并结合星图识别的结果选择部分帧,使用经过改进的OPTICS聚类方法获得目标运动轨迹.最后,使用本文中的算法对软件仿真出的含有目标的高精度星图进行处理验证了算法的可行性.在卫星相对于空间目标抵近过程中,目标检测的水平误差及垂直误差小于0.15°的帧数分别占到了85.4%以及99.6%.相比AVANTI实验中的目标检测方法,减少了在轨任务中相关参数的调节,进一步提升了算法的自主性. 相似文献
2.
Lin Quan Bing Cai Xiong Hu Qingchen Xu Ling Li 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(2):715-721
During solar flares, the X-ray radiation suddenly increases, resulting in an increase in the electron density of the atmospheric D region and a strong absorption of short-wave radio waves. Based on Langfang medium frequency (MF) radar, this paper analyzed the variation characteristics of D region in the lower ionosphere from 62 km to 82 km. The analysis focused on multiple C-level and M-level solar flare events before and after the large-scale flare event at 11:53 (UT) on September 6, 2017. The results show that it is difficult to detect the electron density over 70 km in Langfang during solar flares, but the electron density value can be obtained as low as 62 km, and the stronger the flare intensity, the lower the detectable electron density height. Besides, the equal electron density height, the received power of X and O waves will also be significantly reduced during the flares, and the reduction of equal electron density height has a weak linear relationship with flare intensity. 相似文献
3.
Yongliao Zou Yan Zhu Yunfei Bai Lianguo Wang Yingzhuo Jia Weihua Shen Yu Fan Yang Liu Chi Wang Aibing Zhang Guobin Yu Jihong Dong Rong Shu Zhiping He Tielong Zhang Aimin Du Mingyi Fan Jianfeng Yang Yongqing Peng 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(2):812-823
This paper describes the scientific objectives and payloads of Tianwen-1, China’s first exploration mission to Mars. An orbiter, carrying a lander and a rover, lifted-off in July 2020 for a journey to Mars where it should arrive in February 2021. A suite of 13 scientific payloads, for in-situ and remote sensing, autonomously commanded by integrated payload controllers and mounted on the orbiter and the rover will study the magnetosphere and ionosphere of Mars and the relation with the solar wind, the atmosphere, surface and subsurface of the planet, looking at the topography, composition and structure and in particular for subsurface ice. The mission will also investigate Mars climate history. It is expected that Tianwen-1 will contribute significantly to advance our scientific knowledge of Mars. 相似文献
4.
对一种抽展式火星车转移坡道开展柔顺性优化设计和动力学分析。首先,分析火星车与存在异面角的坡道的挤压几何原理。然后,设计坡道的间隙机构和限位机构,并计算出机构关键设计参数的最优值,以自适应调整两侧坡道的距离,〖JP2〗减小火星车与坡道护栏之间的相互作用力。最后,对坡道下落过程和火星车在坡道上的行驶过程进行动力学仿真,验证坡道柔顺性优化设计的效果。结果表明:优化后的坡道柔顺性大幅提高,坡道可以自适应调整两侧的距离;使用优化后的坡道,可以有效降低火星车与坡道护栏的作用力,实现火星车在坡道上的安全行驶。 相似文献
5.
针对微波电路三维集成结构的迫切需求,开展宽带高集成多级射频互连技术研究。主要设计了两种电路结构,多级水平互连电路与多级垂直互连电路。多级水平互连电路中,通过优化同轴-微带线的水平过渡以及倒角过渡方式,得到在DC~30GHz内的仿真结果,回波损耗优于21dB,插入损耗优于0.16dB;多级垂直互连电路中,通过优化BGA板间互连结构,得到在DC~30GHz内的仿真结果,信号的回波损耗优于13dB,插入损耗优于0.57dB。在小型化、高集成的需求下,宽带高集成多级射频互连技术是解决宽带射频信号传输问题的关键技术路径,可以广泛应用在微波电路三维集成结构中,具有重大的应用前景。 相似文献
6.
7.
Shi Qian Liu James F. Whidborne Lei He 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(3):1174-1187
In the presence of unknown disturbances and model parameter uncertainties, this paper develop a nonlinear backstepping sliding-mode controller (BSMC) for trajectory tracking control of a stratospheric airship using a disturbance-observer (DO). Compared with the conventional sliding mode surface (SMS) constructed by a linear combination of the errors, the new SMS manifold is selected as the last back-step error to improve independence of the adjustment of the controller gains. Furthermore, a nonlinear disturbance-observer is designed to process unknown disturbance inputs and improve the BSMC performances. The closed-loop system of trajectory tracking control plant is proved to be globally asymptotically stable by using Lyapunov theory. By comparing with traditional backstepping control and SMC design, the results obtained demonstrate the capacity of the airship to execute a realistic trajectory tracking mission, even in the presence of unknown disturbances, and aerodynamic coefficient uncertainties. 相似文献
8.
It is difficult to quantitatively detect defects by using the time domain or frequency domain features of Lamb wave signals due to their dispersion and multimodal characteristics.Therefore,it is important to discover an intrinsical parameter of Lamb waves that could be used as a damage sensitive feature.In this paper,quantitative defect detection in aluminium plates is carried out by means of wavenumber analysis approach.The wavenumber of excited Lamb wave mode is a fixed value,given a frequency,a thickness and material properties of the target plate.When Lamb waves propagate to the structural discontinuity,new wavenumber components are created by abrupt wavefield change.The new wavenumber components can be identified in the frequency-wavenumber domain.To estimate spatially dependent wavenumber values,a short-space two-dimensional Fourier transform(FT)method is presented for processing wavefield data of Lamb waves.The results can be used to determine the location,size and depth of rectangular notch.The analysis techniques are demonstrated using simulation examples of an aluminium plate with a rectangular notch.Then,the wavenumber analysis method is applied to simulation data that are obtained through a range of notch depths and widths.The results are analyzed and rules of the technique with regards to estimating notch depth are determined.Based on simulation results,guidelines for using the technique are developed.Finally,experimental wavefield data are obtained in aluminium plates with rectangular notches by a full noncontact transceiving method,i.e.,laser-laser method.Band-pass filtering combined with continuous wavelet transform is used to extract a certain frequency component from the full laser-induced wavefield with wide band.Shortspace two-dimensional FT method is used for further processing full wavefield data at a certain frequency to estimate spatially dependent wavenumber values.The consistency of simulation and experimental results shows the effectiveness of proposed wavenumber method for quantitative rectangular notch detection. 相似文献
9.
Wei LIU Xin MA Ling CHEN Zhenyuan JIA Weixiao LIU Xiao LI Jiakun ZHANG Jiwen LU 《中国航空学报》2018,31(1):89-98
The measurement of position and attitude parameters for the isolated target from a high-speed aircraft is a great challenge in the field of wind tunnel simulation technology. This paper proposes a remote-controlled flexible pose measurement system in wind tunnel conditions for the separation of a target from an aircraft. The position and attitude parameters of a moving object are obtained by utilizing a single camera with a focal length and camera orientation that can be changed based on different measurement conditions. Using this proposed system and method, both the flexibility and efficiency of the pose measurement system can be enhanced in wind tunnel conditions to meet the measurement requirements of different objects and experiments, which is also useful for the development of an intelligent position and attitude measurement system. The position and the focal length of the camera also can be controlled remotely during measurements to enlarge both the vertical and horizontal measurement range of this system. Experiments are conducted in the laboratory to measure the position and attitude of moving objects with high flexibility and efficiency, and the measurement precision of the measurement system is also verified through experiments. 相似文献