首页 | 本学科首页   官方微博 | 高级检索  
文章检索
  按 检索   检索词:      
出版年份:   被引次数:   他引次数: 提示:输入*表示无穷大
  收费全文   335篇
  免费   33篇
  国内免费   35篇
航空   200篇
航天技术   83篇
综合类   27篇
航天   93篇
  2022年   3篇
  2021年   13篇
  2020年   7篇
  2019年   6篇
  2018年   6篇
  2017年   9篇
  2016年   8篇
  2015年   9篇
  2014年   21篇
  2013年   15篇
  2012年   15篇
  2011年   23篇
  2010年   9篇
  2009年   13篇
  2008年   10篇
  2007年   6篇
  2006年   7篇
  2005年   19篇
  2004年   15篇
  2003年   35篇
  2002年   41篇
  2001年   12篇
  2000年   6篇
  1999年   9篇
  1997年   4篇
  1996年   6篇
  1995年   5篇
  1994年   7篇
  1993年   8篇
  1991年   2篇
  1989年   6篇
  1986年   3篇
  1985年   3篇
  1984年   3篇
  1981年   2篇
  1980年   2篇
  1978年   3篇
  1976年   1篇
  1975年   4篇
  1974年   1篇
  1973年   1篇
  1972年   6篇
  1971年   1篇
  1970年   3篇
  1969年   1篇
  1968年   1篇
  1967年   4篇
  1966年   2篇
  1963年   2篇
  1962年   1篇
排序方式: 共有403条查询结果,搜索用时 125 毫秒
81.
关于切顶线三角形有向面积的定值定理及其应用   总被引:1,自引:1,他引:1  
本文给出切顶线三角形(有向)面积的一些定值定理,并据此推出切顶线共点(其中包括射影几何中著名的Brianchon定理在圆外切三角形中的情形)的结论。  相似文献   
82.
83.
84.
在简要介绍了飞行器视觉图像定位导航原理及模型的基础上,针对其非线性模型的推广Kalman滤波的收敛与初始条件有关的问题,将其定位导航的两种模型(线性与非线性模型)组合,提出了双模态双滤波器滤波方法。这种滤波能很好地解决非线性推广Kalman滤波的收敛问题。通过第一个线性滤波器的滤波估计给第二个非线性滤波器提供滤波初值,使这一非线性滤波收敛,并能取得较高的滤波精度。  相似文献   
85.
86.
This paper presents some results of the flight test campaign conducted on the Tecnam P2006T aircraft, on the occasion of its certification process. This twin-engine propeller airplane is certified under the normal category CS-23 and FAR 23. A prototype of this light aircraft has been tested in flight for a post-design performance optimization and for the assessment of flight qualities. These experiences have led to the application of two winglets to the original wing. The final configuration has been extensively tested for the achievement of CS-23 certification. The longitudinal and lateral-directional response modes have been assessed and quantified. At the same time the longitudinal airplane model, through a dedicated set of flight maneuvers, has been characterized by means of parameter estimation studies. The aircraft stability derivatives have been estimated from the acquired flight data using the identification technique known as Output Error Method (OEM). Some estimated stability derivatives have been also compared with the corresponding values extracted from leveled flight tests and from wind tunnel tests performed on a scaled model of the aircraft.  相似文献   
87.
空间核电源热管式辐射散热器热分析与参数优化   总被引:1,自引:0,他引:1       下载免费PDF全文
针对空间热管辐射散热器的特殊工况对散热器进行热分析建模,通过分析其传热原理,建立出热阻模型,并通过和实际设计进行对比,验证模型和计算方法的可行性。选取翅根温度、翅片长度和翅片厚度等参量作为约束条件,分别对热管式空间辐射散热器的翅片散热效率和系统质量特性进行优化分析,获得最优设计参数。  相似文献   
88.
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   
89.
This study reports on ionospheric disturbances that occurred in the early morning hours in the South American–Atlantic sector during a few intense/super storm events. The events were observed at latitudes close to the southern crest of the equatorial ionization anomaly (EIA) as an unusual intensification of the F region electron density peak at local times when the EIA is not usually developed. All the events were observed at pre dawn-morning hours, under conditions of northward interplanetary geomagnetic field. Large scale traveling ionospheric disturbances that are launched during highly disturbed conditions and/or equatorward surges in the thermospheric meridional winds seem to be the most probable causes of the observed disturbances.  相似文献   
90.
We present a comprehensive review of MHD wave behaviour in the neighbourhood of coronal null points: locations where the magnetic field, and hence the local Alfvén speed, is zero. The behaviour of all three MHD wave modes, i.e. the Alfvén wave and the fast and slow magnetoacoustic waves, has been investigated in the neighbourhood of 2D, 2.5D and (to a certain extent) 3D magnetic null points, for a variety of assumptions, configurations and geometries. In general, it is found that the fast magnetoacoustic wave behaviour is dictated by the Alfvén-speed profile. In a ??=0 plasma, the fast wave is focused towards the null point by a refraction effect and all the wave energy, and thus current density, accumulates close to the null point. Thus, null points will be locations for preferential heating by fast waves. Independently, the Alfvén wave is found to propagate along magnetic fieldlines and is confined to the fieldlines it is generated on. As the wave approaches the null point, it spreads out due to the diverging fieldlines. Eventually, the Alfvén wave accumulates along the separatrices (in 2D) or along the spine or fan-plane (in 3D). Hence, Alfvén wave energy will be preferentially dissipated at these locations. It is clear that the magnetic field plays a fundamental role in the propagation and properties of MHD waves in the neighbourhood of coronal null points. This topic is a fundamental plasma process and results so far have also lead to critical insights into reconnection, mode-coupling, quasi-periodic pulsations and phase-mixing.  相似文献   
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号