全文获取类型
收费全文 | 652篇 |
免费 | 140篇 |
国内免费 | 157篇 |
专业分类
航空 | 511篇 |
航天技术 | 140篇 |
综合类 | 124篇 |
航天 | 174篇 |
出版年
2024年 | 3篇 |
2023年 | 9篇 |
2022年 | 33篇 |
2021年 | 43篇 |
2020年 | 38篇 |
2019年 | 38篇 |
2018年 | 29篇 |
2017年 | 37篇 |
2016年 | 37篇 |
2015年 | 41篇 |
2014年 | 68篇 |
2013年 | 26篇 |
2012年 | 48篇 |
2011年 | 54篇 |
2010年 | 39篇 |
2009年 | 55篇 |
2008年 | 38篇 |
2007年 | 38篇 |
2006年 | 23篇 |
2005年 | 40篇 |
2004年 | 32篇 |
2003年 | 17篇 |
2002年 | 21篇 |
2001年 | 21篇 |
2000年 | 14篇 |
1999年 | 12篇 |
1998年 | 18篇 |
1997年 | 15篇 |
1996年 | 8篇 |
1995年 | 5篇 |
1994年 | 7篇 |
1993年 | 9篇 |
1992年 | 7篇 |
1991年 | 10篇 |
1990年 | 9篇 |
1989年 | 4篇 |
1988年 | 2篇 |
1986年 | 1篇 |
排序方式: 共有949条查询结果,搜索用时 15 毫秒
861.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013,52(5):930-935
The high repetition rate satellite laser ranging (SLR) measurements to the fast spinning satellites contain a frequency signal caused by the rotational motion of the corner cube reflector (CCR) array. The spectral filter, developed here, is based on the Lomb algorithm, and is tested with the simulated and the observed high repetition rate SLR data of the geodetic satellite Ajisai (spin period ∼2 s). The filter allows for the noise elimination from the SLR data, and for identification of the returns from the single CCRs of the array – even for the low return rates. Applying the spectral filter to the simulated SLR data increases the S/N ratio by a factor 40–45% for all return rates. Filtering out the noise from the observed data strengthens the frequency signal by factor of ∼25 for the low return rates, which significantly helps to determine the spin phase of the satellite. The spectral filter is applied to the Graz SLR data and the spin rates of Ajisai are determined by two different methods: the frequency analysis and the phase determination of the spinning retroreflector array.The analysis of more than 8 years of the Graz SLR measurements indicates an exponential spin rate trend: f = 0.67034 exp(−0.0148542 Y) [Hz], RMS = 0.085 mHz, where Y is the year since launch. The highly accurate spin rate information demonstrates periodic changes related to the precession of the orbital plane of Ajisai, as it determines the amount of energy received by the satellite from the Sun. The rate of deceleration of Ajisai is not constant: the half life period of the satellite’s spin oscillates around 46.7 years with an amplitude of about 5 years. 相似文献
862.
介绍了美国空军2010年发布的"技术地平线"的出台背景、主要内容.并根据该研究报告浅析了美国空军未来的装备与技术趋向. 相似文献
863.
通过一种典型的冷却方案介绍热电制冷在激光器冷却系统中的应用,提出了以实验数据指导冷却方案设计,以热仿真手段进一步优化冷却方案,最终通过热测试技术验证冷却系统是否满足激光器的实际工作要求的三步走设计方法,该方法提高了热电制冷方案设计效率,为激光器冷却系统系列化、模块化打下基础。 相似文献
864.
D. Kucharski G. Kirchner F. Koidl E. Cristea 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009,43(12):1926-1930
Satellite Laser Ranging (SLR) stations measure distance to the satellites equipped with Corner Cube Reflectors (CCRs). These range measurements contain information about spin parameters of the spacecraft. In this paper we present results of spin period determination of two passive satellites from SLR data only: 10 years of LAGEOS-1 (10426 values), and 15 years of LAGEOS-2 (15580 values). The measurements have been made by standard 10 Hz SLR systems and the first 2 kHz SLR system from Graz (Austria). The obtained data allowed calculation of the initial spin period of the satellites: 0.61 s for LAGEOS-1 and 0.906 s for LAGEOS-2. Long time series of the spin period values show that the satellite’s slowing down rate is not constant but is oscillating with a period of 846 days for LAGEOS-1 and 578 days for LAGEOS-2. The results presented here definitely prove that the SLR is a very efficient technique able to measure spin period of the geodetic satellites. 相似文献
865.
Wendong Meng Haifeng Zhang Peicheng Huang Jie Wang Zhongping Zhang Ying Liao Yang Ye Wei Hu Yuanming Wang Wanzhen Chen Fumin Yang Ivan Prochazka 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
High-precision time synchronization between satellites and ground stations plays the vital role in satellite navigation system. Laser time transfer (LTT) technology is widely recognized as the highest accuracy way to achieve time synchronization derived from satellite laser ranging (SLR) technology. Onboard LTT payload has been designed and developed by Shanghai Astronomical Observatory, and successfully applied to Chinese Beidou navigation satellites. By using the SLR system, with strictly controlling laser firing time and developing LTT data processing system on ground, the high precise onboard laser time transfer experiment has been first performed for satellite navigation system in the world. The clock difference and relative frequency difference between the ground hydrogen maser and space rubidium clocks have been obtained, with the precision of approximately 300 ps and relative frequency stability of 10E−14. This article describes the development of onboard LTT payload, introduces the principle, system composition, applications and LTT measuring results for Chinese satellite navigation system. 相似文献
866.
精密钣金成形技术在航空制造领域的应用分析 总被引:2,自引:0,他引:2
介绍了钣金成形技术的发展和精密钣金成形技术的应用,并对精密钣金成形技术过程中的关键技术和发展方向进行了分析。 相似文献
867.
633nm碘稳定激光器作为长度基(标)准的比对测量 总被引:1,自引:0,他引:1
简述作为长度基(标)准用的633nm碘稳定激光器的技术指标以及它的测量方法,文中以作者所进行的国际和国内比对中的测量结果为例,给出了这类激光器可以复现的频率或波长不确定度。 相似文献
868.
869.
1.前言 激光跟踪系统是航空航天工程中的重要设备之一。要想建造高精度激光跟踪系统,除了提高有关部件的精度之外,系统的综合设计是一个关键步骤。对于这类系统的综合设计,目前都采用全连续或全离散控制方案,而且不考虑对象未建模动态和子系统间的耦合问题。 相似文献
870.
1420铝锂合金薄板激光焊接头的撕裂韧性研究 总被引:3,自引:0,他引:3
对 1420铝锂合金及其激光焊接头的撕裂韧性进行了研究。试验按照美国材料试验学会ASTMB871—01《铝合金产品撕裂试验标准》进行。同时调查了铝合金及激光焊接接头的硬度分布及显微组织。撕裂试验表明,所有试样的启裂能均高于裂纹扩展能。不论启裂能还是裂纹扩展能,基材均高于焊缝及热影响区,基材L T方向高于T L方向。断口观察发现,基材的断口表面,特别是T L方向存在长而深的撕裂凹槽,焊缝及热影响区试样表面主要是沿晶或沿亚晶的脆性断口。由基材的高韧性到焊缝与热影响区的低韧性,是由于发生了断裂模式的转变,发生了由延性断裂向沿晶脆性断裂的转变。 相似文献