全文获取类型
收费全文 | 370篇 |
免费 | 50篇 |
国内免费 | 30篇 |
专业分类
航空 | 109篇 |
航天技术 | 148篇 |
综合类 | 11篇 |
航天 | 182篇 |
出版年
2023年 | 8篇 |
2022年 | 18篇 |
2021年 | 17篇 |
2020年 | 18篇 |
2019年 | 13篇 |
2018年 | 8篇 |
2017年 | 4篇 |
2016年 | 5篇 |
2015年 | 12篇 |
2014年 | 21篇 |
2013年 | 13篇 |
2012年 | 21篇 |
2011年 | 31篇 |
2010年 | 19篇 |
2009年 | 20篇 |
2008年 | 23篇 |
2007年 | 34篇 |
2006年 | 27篇 |
2005年 | 9篇 |
2004年 | 15篇 |
2003年 | 13篇 |
2002年 | 12篇 |
2001年 | 14篇 |
2000年 | 10篇 |
1999年 | 10篇 |
1998年 | 12篇 |
1997年 | 6篇 |
1996年 | 7篇 |
1995年 | 5篇 |
1994年 | 8篇 |
1993年 | 1篇 |
1992年 | 7篇 |
1991年 | 2篇 |
1990年 | 5篇 |
1989年 | 1篇 |
1987年 | 1篇 |
排序方式: 共有450条查询结果,搜索用时 15 毫秒
251.
252.
针对传统单目视觉里程计存在的尺度漂移和尺度不一致问题,提出了一种基于无监督深度学习的单目视觉里程计。首先,联合使用空间几何约束和图像相似性约束,得到长序列尺度一致的深度估计网络和鲁棒的光流估计网络;然后,对密集光流进行采样,得到精确的稀疏对应关系,减少尺度漂移;最后,根据改进的ORB-SLAM初始化方法,选择最优跟踪方式,结合深度信息进行尺度对齐,从而得到全局尺度一致的视觉里程计。在KITTI数据集上进行大量实验,结果表明,相较于ORB-SLAM2和基于深度学习的端到端的视觉里程计系统,该算法在通用评估指标方面性能有明显提升,验证了该算法的有效性。 相似文献
253.
成像光谱技术超谱图像分类研究现状与分析 总被引:13,自引:0,他引:13
超谱遥感图像由于其高光谱分辨率的特点正受到国外内的广泛关注,在解决了前期的辐射校正及定标等剖以及,超谱图像的推广应用是当务之急。超谱遥感图像的分类研究对农作物生长状况的监测、矿物的识别、海洋水色分析以及其他方面的许多应用都是很有价值的。文章概述了国内外在成像光谱技术方面的发展,并首次以像元的构成成分的.纯像元和混合像元的角度对分类方法进行了论述,对超谱图像分类技术研究现状的归纳和分析,旨在寻找突破点,加强此领域的研究力度。 相似文献
254.
《中国航空学报》2016,(6):1806-1814
Inspection techniques for aero-engine blades are a hot topic in industry. Since these blades have a sculptured surface and a small datum, measurement results may deviate from an actual position. There are few proper approaches compensating for non-uniform distribution errors that are within specified tolerance ranges. This study aimed to develop a meshing structure measur-ing approach for the distortion of blades via non-contact optical 3D scanning. A rough measure-ment and a registration procedure are initially adopted to rectify the coordinate system of a blade, which avoids the initial coordinate system errors caused by the small datum. A measurement path with meshing structure is then unfolded on the blade surface. For non-uniform distribution errors, the meshing structure measurement is more visual and clear than the traditional constant height curves method. All measuring points take only 7 min to complete, and the distribution of error is directly and accurately presented by the meshing structure. This study provides a basis for future research on distortion control and error compensation. 相似文献
255.
256.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2020,65(5):1333-1343
This paper investigates the motion control system of an optical telescope system used for precision satellite tracking and ranging applications. The system uses direct-drive permanent magnet synchronous motors (PMSMs) for high precision positioning. To overcome the performance limitations due to system dynamics and position dependent plant variations, a disturbance observer based control system is utilized. This paper contributes the detailed analysis, design and implementation of such an advanced control concept for the performance improvement of precision satellite tracking systems. Satellite tracking experiments are conducted to verify the performance of the proposed system. Utilizing the proposed control concept, the RMS servo error is reduced by a factor of 3.8 to well below the arcsecond range, achieving seeing limited tracking. 相似文献
257.
258.
Paweł Lejba Tomasz Suchodolski Piotr Michałek Jacek Bartoszak Stanisław Schillak Stanisław Zapaśnik 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(10):2609-2616
The Borowiec Satellite Laser Ranging station (BORL 7811, Borowiec) being a part of the Space Research Centre of the Polish Academy of Sciences (SRC PAS) went through modernization in 2014–2015. One of the main tasks of the modernization was the installation of a high-energy laser module dedicated to space debris tracking. Surelite III by Continuum is a Nd:YAG pulse laser with 10?Hz repetition rate, a pulse width of 3–5?ns and a pulse energy of 450?mJ for green (532?nm). This new laser unit was integrated with the SLR system at Borowiec performing standard satellite tracking. In 2016 BORL 7811 participated actively to the observational campaigns related to the space debris targets from LEO region managed by the Space Debris Study Group (SDSG) of the International Laser Ranging Service (ILRS).Currently, Borowiec station regularly tracks 36 space debris from the LEO regime, including typical rocket bodies (Russian/Chinese) and cooperative targets like the inactive TOPEX/Poseidon, ENVISAT, OICETS and others. In this paper the first results of space debris laser measurements obtained by the Borowiec station in period August 2016 – January 2017 are presented. The results gained by the SRC PAS Borowiec station confirm the rotation of the defunct TOPEX/Poseidon satellite which spins with a period of approximately 10?s. The novelty of this work is the presentation of the sample results of the Chinese CZ-2C R/B target (NORAD catalogue number 31114) which is equipped (probably) with retroreflectors. Laser measurements to space debris is a very desirable topic for the next years, especially in the context of the Space Surveillance and Tracking (SST) activity. Some targets are very easy to track like defunct ENVISAT or TOPEX/Poseidon. On the other hand, there is a big population of different LEO targets with different orbital and physical parameters, which are challenging for laser ranging like small irregular debris and rocket boosters. 相似文献
259.
空间光学遥感器光机结构材料应用情况及展望 总被引:2,自引:0,他引:2
介绍了空间光学遥感器的技术特点,综述了近年来空间光学遥感器光机结构材料的应用状况,对空间光学遥感器的光机结构材料发展趋势进行了展望。 相似文献
260.
Masahiko Uetsuhara Toshiya Hanada 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
Identifying spacecraft breakup events is an essential issue for better understanding of the current orbital debris environment. This paper proposes an observation planning approach to identify an orbital anomaly, which appears as a significant discontinuity in archived orbital history, as a spacecraft breakup. The proposed approach is applicable to orbital anomalies in the geostationary region. The proposed approach selects a spacecraft that experienced an orbital anomaly, and then predicts trajectories of possible fragments of the spacecraft at an observation epoch. This paper theoretically demonstrates that observation planning for the possible fragments can be conducted. To do this, long-term behaviors of the possible fragments are evaluated. It is concluded that intersections of their trajectories will converge into several corresponding regions in the celestial sphere even if the breakup epoch is not specified and it has uncertainty of the order of several weeks. 相似文献