全文获取类型
收费全文 | 483篇 |
免费 | 124篇 |
国内免费 | 18篇 |
专业分类
航空 | 165篇 |
航天技术 | 415篇 |
综合类 | 4篇 |
航天 | 41篇 |
出版年
2023年 | 17篇 |
2022年 | 17篇 |
2021年 | 35篇 |
2020年 | 38篇 |
2019年 | 27篇 |
2018年 | 23篇 |
2017年 | 18篇 |
2016年 | 8篇 |
2015年 | 8篇 |
2014年 | 49篇 |
2013年 | 68篇 |
2012年 | 41篇 |
2011年 | 52篇 |
2010年 | 22篇 |
2009年 | 42篇 |
2008年 | 34篇 |
2007年 | 17篇 |
2006年 | 10篇 |
2005年 | 17篇 |
2004年 | 11篇 |
2003年 | 12篇 |
2002年 | 5篇 |
2001年 | 5篇 |
2000年 | 3篇 |
1999年 | 7篇 |
1998年 | 6篇 |
1997年 | 6篇 |
1996年 | 5篇 |
1995年 | 4篇 |
1994年 | 6篇 |
1993年 | 5篇 |
1992年 | 2篇 |
1991年 | 2篇 |
1990年 | 1篇 |
1987年 | 2篇 |
排序方式: 共有625条查询结果,搜索用时 11 毫秒
171.
Biswajit Sahu Mouloud Tribeche 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
The properties of cylindrical and spherical electron acoustic shock waves (EASWs) in an unmagnetized plasma consisting of cold electrons, immobile ions and Boltzmann distributed hot electrons are investigated by employing the reductive perturbation method. A Korteweg–de Vries Burgers (KdVB) equation is derived and its numerical solution is obtained. The effects of several parameters and ion kinematic viscosity on the basic features of EA shock waves are discussed in nonplanar geometry. It is found that nonplanar EA shock waves behave quite differently from their one-dimensional planar counterpart. 相似文献
172.
介绍了中国科学院国家空间科学中心新建成的空间电子辐射环境探测载荷测试定标试验平台.该平台由中、高能极弱流电子加速器以及内置多维真空转台的真空靶室试验终端组成,用于对星载空间电子辐射探测器进行地面加速器测试定标.重点描述了为得到中能极弱流均匀平行束,采用电子轨迹程序Egun对中能极弱流电子加速器进行的物理设计和模拟计算,给出球形结构电子枪在栅网孔不加栅网、加理想栅网和直径1mm孔栅网以及在不同加速管出口能量情况下,初聚系统和加速管以及经过二次扩束时输运段中电子轨迹的模拟结果.最终得出能够实现电子枪初始束流减弱8个数量级,获得满足测试定标试验需求的极弱流均匀平行电子束(在试验终端直径50mm靶上束流面密度为105~109cm-2·s-1)的结论. 相似文献
173.
Vishal Chauhan O.P. Singh 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
The temporal and seasonal variations of Total Electron Content (TEC) are studied at Agra (Geographic Lat. 27.17°N, Long. 78.89°E, Dip: 41.4°), India, which is in the equatorial anomaly region, for a period of 12 months from 01 January to 31 December, 2007 using a Global Positioning System (GPS) receiver. The mean TEC values show a minimum at 0500 h LT (LT = UT + 5.5 h) and a peak value at about 1400 h LT. The lowest TEC values are observed in winter whereas largest values are observed in equinox and summer. Anomalous variations are found during the period of magnetic disturbances. These results are compared with the TEC derived from IRI-2007 using three different options of topside electron density, NeQuick, IRI01-corr, and IRI-2001. A good agreement is found between the TEC obtained at Agra and those derived from IRI models. 相似文献
174.
TEC计算方法探讨和赤道异常北驼峰时空特征测量初析 总被引:1,自引:0,他引:1
本文探讨了应用最小曲率原理由单站微分多普勒频移数据计算TEC时所遇到的问题和解决办法。处理了用MX1502大地定位接收机于1989年8月和9月先后在陕西临潼和北京观测的NNSS卫星多普勒频移数据,得到了TEC时空分布曲线。分析这些曲线,得到了TEC赤道异常北驼峰时空特征在太阳活动高年(尤其是8月中旬太阳特大质子事件中)的某些结果。 相似文献
175.
常规的电推进技术是针对大卫星应用而研制的,体积大、功耗高,不能满足小卫星飞速发展的实际需要。针对小卫星对电推进器的要求,提出了利用电子回旋谐振微波放电技术,采用微波同轴放电腔体的小型化离子推进器。由于同轴传输线不存在截止波长,放电腔体的直径选择非常灵活,可以适应小卫星的低供电能力和对体积重量的要求。实验样机的直径为50mm,在微波功率为30W,加速电压1.2kV,减速电压0.2kV的条件下,等离子体的电子密度达到了4.6×10^16/m^3,推进器的离子束流也达到6mA。实验样机的体积大大低于常规波导谐振腔微波离子推进器,实现了小型化,基本满足了小卫星对电推进器的体积重量要求。 相似文献
176.
研究了电子束快速成形TC18钛合金(简称KTC 18)3种典型退火制度下显微组织演化规律及与显微硬度的关系.结果表明,在700~830℃单一退火条件下,合金相组成为初生α相与亚稳β相,随着温度升高,初生α相体积分数减少,基体显微硬度变化较小;在双重退火条件下,500~650℃之间低温退火过程中会析出细小、编织排列的条状α相,可显著提高基体硬度,随着低温退火温度升高,α析出相粗化且数量变少,导致基体硬度降低;三重退火条件下,高温炉冷和中温退火过程中会产生粗大的竹叶状一次α相,其数量随中温退火温度升高而减少,对显微硬度影响较小.低温退火析出的细小、弥散α相对KTC 18显微硬度影响最大,其数量和尺寸取决于其他类型α相的数量和低温退火制度. 相似文献
177.
Zhinmin Liu Yangyang Li Fei Li Jinyun Guo 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(6):1435-1443
Ionosphere delay is very important to GNSS observations, since it is one of the main error sources which have to be mitigated even eliminated in order to determine reliable and precise positions. The ionosphere is a dispersive medium to radio signal, so the value of the group delay or phase advance of GNSS radio signal depends on the signal frequency. Ground-based GNSS stations have been used for ionosphere monitoring and modeling for a long time. In this paper we will introduce a novel approach suitable for single-receiver operation based on the precise point positioning (PPP) technique. One of the main characteristic is that only carrier-phase observations are used to avoid particular effects of pseudorange observations. The technique consists of introducing ionosphere ambiguity parameters obtained from PPP filter into the geometry-free combination of observations to estimate ionospheric delays. Observational data from stations that are capable of tracking the GPS/BDS/GALILEO from the International GNSS Service (IGS) Multi-GNSS Experiments (MGEX) network are processed. For the purpose of performance validation, ionospheric delays series derived from the novel approach are compared with the global ionospheric map (GIM) from Ionospheric Associate Analysis Centers (IAACs). The results are encouraging and offer potential solutions to the near real-time ionosphere monitoring. 相似文献
178.
I.P. Gabis 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
Equatorial total column ozone variations with quasi-biennial periodicity are described by paying attention to their coupling with the quasi-biennial oscillation (QBO) of zonal wind in equatorial stratosphere. Analysis is made for the 35-year time interval from 1978 to 2013 using the zonal mean total ozone (TOZ) data in latitude band from 5° S to 5° N derived from satellite measurements by means of Total Ozone Mapping Spectrometer (TOMS) and Ozone Monitoring Instrument (OMI). The study was performed using strong seasonal regularities of the wind QBO and the discrete variation of the QBO-period revealed earlier. The forecast of the wind QBO evolution made in Gabis (2012) is fully justified. The comparison between predicted and actually observed changes of the height wind structure shows the prominent accordance, which confirms the forecast validity. It is shown that variations of deseasonalized TOZ are in strong coupling with changes of equatorial wind QBO that coincides with the numerous previous researches. However our results contradict the assumption about quite complicated ozone response in the equatorial region due to continuously varying with time relationship between annual and quasi-biennial cycles and irregularly variable wind QBO-period. The total ozone changes actually observed clearly corresponds to the mean ozone variations calculated for different QBO scenarios and aligned according to the sequence of QBO scenarios already occurred in fact. This close association indicates the possibility of forecasting the equatorial total ozone QBO based on the predicted wind QBO. 相似文献
179.
First results of operational ionospheric dynamics prediction for the Brazilian Space Weather program
Adriano Petry Jonas Rodrigues de Souza Haroldo Fraga de Campos Velho André Grahl Pereira Graham John Bailey 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
It is shown the development and preliminary results of operational ionosphere dynamics prediction system for the Brazilian Space Weather program. The system is based on the Sheffield University Plasmasphere–Ionosphere Model (SUPIM), a physics-based model computer code describing the distribution of ionization within the Earth mid to equatorial latitude ionosphere and plasmasphere, during geomagnetically quiet periods. The model outputs are given in a 2-dimensional plane aligned with Earth magnetic field lines, with fixed magnetic longitude coordinate. The code was adapted to provide the output in geographical coordinates. It was made referring to the Earth’s magnetic field as an eccentric dipole, using the approximation based on International Geomagnetic Reference Field (IGRF-11). During the system operation, several simulation runs are performed at different longitudes. The original code would not be able to run all simulations serially in reasonable time. So, a parallel version for the code was developed for enhancing the performance. After preliminary tests, it was frequently observed code instability, when negative ion temperatures or concentrations prevented the code from continuing its processing. After a detailed analysis, it was verified that most of these problems occurred due to concentration estimation of simulation points located at high altitudes, typically over 4000 km of altitude. In order to force convergence, an artificial exponential decay for ion–neutral collisional frequency was used above mentioned altitudes. This approach shown no significant difference from original code output, but improved substantially the code stability. In order to make operational system even more stable, the initial altitude and initial ion concentration values used on exponential decay equation are changed when convergence is not achieved, within pre-defined values. When all code runs end, the longitude of every point is then compared with its original reference station longitude, and differences are compensated by changing the simulation point time slot, in a temporal adjustment optimization. Then, an approximate neighbor searching technique was developed to obtain the ion concentration values in a regularly spaced grid, using inverse distance weighting (IDW) interpolation. A 3D grid containing ion and electron concentrations is generated for every hour of simulated day. Its spatial resolution is 1° of latitude per 1° of longitude per 10 km of altitude. The vertical total electron content (VTEC) is calculated from the grid, and plotted in a geographic map. An important feature that was implemented in the system is the capacity of combining observational data and simulation outputs to obtain more appropriate initial conditions to the ionosphere prediction. Newtonian relaxation method was used for this data assimilation process, where ionosonde data from four different locations in South America was used to improve the system accuracy. The whole process runs every day and predicts the VTEC values for South America region with almost 24 h ahead. 相似文献
180.
2009年7月22日日全食期间电离层参量的变化 总被引:1,自引:2,他引:1
利用多个电离层垂测站的数据和IGS-TEC数据资料, 结合日地空间环境指数, 分析了2009年7月22日日全食期间中国地区电离层参量(反射回波最低频率fmin及f0F2和TEC)的变化特征. 结果表明, 日食发生后fmin迅速降低, 日食结束后fmin迅速恢复到正常水平; 在食甚时刻附近, f0F2和TEC出现明显的降低, 显示了明显的光食效应. 日食结束后5~6 h, f0F2和TEC出现不同程度的正扰动, 在驼峰区更明显; 日食结束后9~10 h, f0F2和TEC出现较显著的负扰动. 由于此次日食发生时伴随着中等强度的磁暴和低纬电场穿透等空间天气事件, 给此次日食电离层效应的深入分析带来很大困难. 相似文献