全文获取类型
收费全文 | 254篇 |
免费 | 69篇 |
国内免费 | 20篇 |
专业分类
航空 | 115篇 |
航天技术 | 156篇 |
综合类 | 3篇 |
航天 | 69篇 |
出版年
2024年 | 2篇 |
2023年 | 20篇 |
2022年 | 15篇 |
2021年 | 39篇 |
2020年 | 23篇 |
2019年 | 23篇 |
2018年 | 21篇 |
2017年 | 12篇 |
2016年 | 8篇 |
2015年 | 9篇 |
2014年 | 21篇 |
2013年 | 31篇 |
2012年 | 12篇 |
2011年 | 41篇 |
2010年 | 13篇 |
2009年 | 9篇 |
2008年 | 7篇 |
2007年 | 6篇 |
2006年 | 7篇 |
2005年 | 2篇 |
2004年 | 2篇 |
2003年 | 5篇 |
2002年 | 3篇 |
2001年 | 2篇 |
2000年 | 2篇 |
1998年 | 3篇 |
1996年 | 4篇 |
1991年 | 1篇 |
排序方式: 共有343条查询结果,搜索用时 15 毫秒
191.
A. von Engeln Y. AndresC. Marquardt F. Sancho 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
The GRAS radio occultation instrument is flying on Metop-A and belongs to the EPS (EUMETSAT Polar System). GRAS observes GPS satellites in occultation. Within this work, validation of GRAS closed-loop bending angle data against co-located ECMWF profiles extracted from model fields and occultations from the COSMIC constellation of radio occultation instruments is shown. Results confirm the high data quality and robustness, where GRAS shows lower bending angle noise against ECMWF than COSMIC and in terms of occultations per day, one GRAS ≈ two COSMIC satellites. This is partly due to the operational setup of EPS. For the investigation we focus on two observation periods where updates in the ECMWF (March 2009) and COSMIC processing (October 2009) have improved the statistics further. Bending angles biases agree to within 0.5% against ECMWF and to within 0.1% against COSMIC after the updates for altitudes between 8 and 40 km. In addition, we also analyze the impact of the Metop orbit processing on the derived GRAS bending angle data, where different GPS and Metop orbit solutions are analyzed. Results show that a batch based orbit processing would improve in particular the bending angle bias behavior at higher altitudes. Requirements for the operational processing of GRAS data are briefly outlined, options to ease the use of other positioning system satellites in the near future are discussed. A simplified analysis on the observation of several of these systems, e.g. GPS and Galileo, from one platform shows that about 16% of occultations are found within 300 km, ±3 h, thus providing similar information. A constellation of 2 GRAS like instruments would have only about 10% close-by. 相似文献
192.
L. Alfonsi L. Spogli J.R. Tong G. De Franceschi V. Romano A. Bourdillon M. Le Huy C.N. Mitchell 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
We use observations of ionospheric scintillation at equatorial latitudes from two GPS receivers specially modified for recording, at a sampling rate of 50 Hz, the phase and the amplitude of the L1 signal and the Total Electron Content (TEC) from L1 and L2. The receivers, called GISTM (GPS Ionospheric Scintillation and TEC Monitor), are located in Vietnam (Hue, 16.4°N, 107.6°E; Hoc Mon, 10.9°N, 106.6°E). These experimental observations are analysed together with the tomographic reconstruction of the ionosphere produced by the Multi-Instrument Data Analysis System (MIDAS) for investigating the moderate geomagnetic storm which occurred on early April 2006, under low solar activity. The synergic adoption of the ionospheric imaging and of the GISTM measurements supports the identification of the scale-sizes of the ionospheric irregularities causing scintillations and helps the interpretation of the physical mechanisms generating or inhibiting the appearance of the equatorial F layer irregularities. In particular, our study attributes to the turning of the IMF (Interplanetary Magnetic Field) between northward and southward direction an important role in the inhibition of the generation of spread F irregularities resulting in a lack of scintillation enhancement in the post-sunset hours. 相似文献
193.
U. Weinbach S. Schön 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
Processing data from Global Navigation Satellite Systems (GNSS) always requires time synchronization between transmitter and receiver clocks. Due to the limited stability of the receiver’s internal oscillator, the offset of the receiver clock with respect to the system time has to be estimated for every observation epoch or eliminated by processing differences between simultaneous observations. If, in contrast, the internal oscillator of the receiver is replaced by a stable atomic clock one can try to model the receiver clock offset, instead of estimating it on an epoch-by-epoch basis. In view of the progress made in the field of high-precision frequency standards we will investigate the technical requirements for GNSS receiver clock modeling at the carrier phase level and analyze its impact on the precision of the position estimates. 相似文献
194.
R. Pacione B. Pace H. Vedel S. de Haan R. Lanotte F. Vespe 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
In this article we present two methods for combination of different Global Navigation Satellite Systems (GNSS) Zenith Total Delay (ZTD) time-series for the same GNSS site, but from different producers or different processing setups. One method has been setup at ASI/CGS, the other at KNMI. Using Near Real-Time (NRT) ZTD data covering 1 year from the E-GVAP project, the performance of the two methods is inter-compared and validation is made against a combined ZTD solution from EUREF, based on post-processed ZTDs. Further, validation of the ASI combined solutions is made against independent ZTDs derived from radiosonde, Numerical Weather Prediction (NWP) model and Very Long Baseline Interferometry (VLBI) ZTD. 相似文献
195.
Florent Deleflie Alessandro Rossi Christophe Portmann Gilles Métris François Barlier 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
This paper aims at investigating the stability over 150 years of a very large number of trajectories in the Medium Earth Orbit (MEO) region, near the orbits devoted to radionavigation such as the Global Navigation Satellite Systems (GNSS like GPS, Glonass, Galileo, COMPASS). 相似文献
196.
197.
作为星载掩星技术的推广,基于飞机平台的无线电掩星技术备受关注。为了将机栽掩星技术更好地应用到工程实践中,文章通过介绍机载掩星探测的基本原理和主要特点、模拟仿真,对机载掩星的反演算法进行了探讨,并给出模拟结果:包括利用STK仿真软件生成仿真场景;采用3维射线追踪技术模拟机载无线电掩星,预报掩星事件出现的时间、仰角,模拟信号传播特征;详细研究大气层内折射率反演技术并给出反演结果。研究结果表明,模拟仿真对机载掩星工程化实现是有益的。最后展望了机载掩星探测的发展趋势,提出了弱掩星信号的捕获跟踪、飞机平台的精度定位测速以及反射信号的抗干扰三项技术及工程化中需解决的技术难点。 相似文献
198.
提出了一种以星上有效载荷的形式搭载在低轨综合卫星平台上的PNT服务系统,可作为GNSS系统的补充、备份和验证手段。本文总结了低轨卫星PNT服务的发展现状,提出了该低轨PNT服务系统的设计方案和总体架构,分析了系统的工作原理、服务性能以及对GNSS系统的可补充和验证性。最后给出了系统建设需要研究的几项关键技术,初步论证了该PNT系统的可行性和技术可实现性。 相似文献
199.
200.
矩形波导内的微放电效应 总被引:1,自引:1,他引:0
分析了空间射频系统中微波放电现象。采用数值方式对距形波导内传输不同模式场时的微放电特性进行了计算,并进行了简单的比较。论述了抑制微波放电的措施。结果表明,在射频系统中,当传输的是行波场时,微放电的危害相对较大。而采用微扰磁场技术可以有效的抑制微放电的强度。 相似文献