全文获取类型
收费全文 | 3217篇 |
免费 | 640篇 |
国内免费 | 573篇 |
专业分类
航空 | 2941篇 |
航天技术 | 423篇 |
综合类 | 374篇 |
航天 | 692篇 |
出版年
2024年 | 9篇 |
2023年 | 53篇 |
2022年 | 83篇 |
2021年 | 147篇 |
2020年 | 141篇 |
2019年 | 135篇 |
2018年 | 120篇 |
2017年 | 175篇 |
2016年 | 184篇 |
2015年 | 172篇 |
2014年 | 233篇 |
2013年 | 194篇 |
2012年 | 232篇 |
2011年 | 266篇 |
2010年 | 204篇 |
2009年 | 212篇 |
2008年 | 200篇 |
2007年 | 253篇 |
2006年 | 209篇 |
2005年 | 206篇 |
2004年 | 151篇 |
2003年 | 150篇 |
2002年 | 119篇 |
2001年 | 102篇 |
2000年 | 109篇 |
1999年 | 72篇 |
1998年 | 62篇 |
1997年 | 53篇 |
1996年 | 34篇 |
1995年 | 32篇 |
1994年 | 23篇 |
1993年 | 25篇 |
1992年 | 21篇 |
1991年 | 12篇 |
1990年 | 16篇 |
1989年 | 11篇 |
1988年 | 4篇 |
1987年 | 3篇 |
1986年 | 2篇 |
1984年 | 1篇 |
排序方式: 共有4430条查询结果,搜索用时 125 毫秒
991.
空中交通管制员不安全行为纠正 总被引:1,自引:0,他引:1
为减少因空中交通管制员的不安全行为所导致的不安全事件,依据空中交通管制工作特点,应用不安全行为纠正技术,建立管制员不安全行为纠正实施的规则与实施计划,针对10位管制员进行16周的行为观察与纠正,其整体安全行为指数由65.82%提高到72.79%,取得预期效果。在管理制度和硬件系统不断完善的情况下,该方法可以作为一种提高管制质量的有效途径。 相似文献
992.
Iu.V. Cherniak I.E. Zakharenkova A. Krankowski I.I. Shagimuratov 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
The plasmaspheric electron content (PEC) was estimated by comparison of GPS TEC observations and FORMOSAT-3/COSMIC radio occultation measurements at the extended solar minimum of cycle 23/24. Results are retrieved for different seasons (equinoxes and solstices) of the year 2009. COSMIC-derived electron density profiles were integrated up to the height of 700 km in order to retrieve estimates of ionospheric electron content (IEC). Global maps of monthly median values of COSMIC IEC were constructed by use of spherical harmonics expansion. The comparison between two independent measurements was performed by analysis of the global distribution of electron content estimates, as well as by selection specific points corresponded to mid-latitudes of Northern America, Europe, Asia and the Southern Hemisphere. The analysis found that both kinds of observations show rather similar diurnal behavior during all seasons, certainly with GPS TEC estimates larger than corresponded COSMIC IEC values. It was shown that during daytime both GPS TEC and COSMIC IEC values were generally lower at winter than in summer solstice practically over all specific points. The estimates of PEC (h > 700 km) were obtained as a difference between GPS TEC and COSMIC IEC values. Results of comparative study revealed that for mid-latitudinal points PEC estimates varied weakly with the time of a day and reached the value of several TECU for the condition of solar minimum. Percentage contribution of PEC to GPS TEC indicated the clear dependence from the time with maximal values (more than 50–60%) during night-time and lesser values (25–45%) during day-time. 相似文献
993.
Shridhar D. Jawak Alvarinho J. Luis 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
An enhanced digital elevation model (DEM) of the Larsemann Hills region, east Antarctica, is constructed synergistically by using highly accurate ground-based GPS measurements, satellite-derived laser altimetry (GLAS/ICESat) and Radarsat Antarctic Mapping Project (RAMPv2) DEM-based point elevation dataset. Our DEM has a vertical accuracy of about 1.5 times better than RAMPv2 DEM and seven times better than GLAS/ICESAT-based DEM. The accuracy is improved by validating the RAMPv2 DEM elevation by supplementing with GLAS/ICESat and DGPS survey data, when compared to that of DEM constructed by using GLAS/ICESat or RAMPv2 alone. With the use of accurate GPS data as ground control points reference elevations, the DEM extracted is much more accurate with least mean RMSE of 34.5 m than that constructed by using a combination of GLAS/ICESat and RAMPv2 as true reference. The newly constructed DEM 7 achieves highest accuracy with the least average elevation difference of 0.27 m calculated using 46 ground reference points. Available DEMs of Antarctic region generated by using radar altimetry and the Antarctic Digital Database indicate elevation variations in the range of 50–100 m, which necessitates the generation of local DEM and its validation by using ground truth. This is our first attempt of fusing multi-temporal, multi-sensor and multi-source elevation data to generate a DEM of any part of Antarctica, in order to address the ice elevation change to infer the ice mass balance. Our approach focuses on the strengths of each elevation data source to produce an accurate DEM. 相似文献
994.
995.
996.
介绍利用单片单板机接口电路完成对6V、30W白炽灯光源与其对应的标准白炽灯光源的色温比对标定工作。 相似文献
997.
防空导弹武器兵力分配优化模型 总被引:2,自引:0,他引:2
高尚 《南京航空航天大学学报》2000,32(3)
兵力优化分配是防空作战部署中的重要问题。文中利用排队论、对策论理论和方法 ,研究了防空导弹兵力分配问题 ,建立了防空导弹兵力分配优化模型及其解法。给出了一个实例 ,并用线性规划方法得到了最优混合策略。最后讨论了实战中的情况与基本假设不符合时的解决方法。对于多通道的导弹武器部署问题可用类似的方法处理 ,此方法为防空导弹部署优化提供了一个基本思路。 相似文献
998.
对将增强碳/碳纤维块体切削成球锥外形的工艺,块体热膨胀系数异性轴指向可以极大地影响球锥热应力大小,存在优化设计的潜力。本文对增强碳/碳不同主轴方向弹性模量比值下的球锥最小热应力优化特性进行了研究,发现以1为界,不同模量对比关系下的优化特征是完全不同的。在本文加热条件下,当异性轴模量小于同性面模量时,优化曲线对温度场变化很敏感,以块体异性轴和球锥横截面成±42.9夹角时热应力最小;当异性轴模量大于同性面模量时,优化曲线随加热时间变化不大,以块体同性面与球锥对称轴平行或成小锐角时热应力最小。一般而言,工艺设计中应避免用模量大的主轴方向指向球锥对称轴方向。 相似文献
999.
随着空中交通流量的日渐增大,空域结构及交通流分布的不合理性导致空中交通管制与飞行安全存在着一定的隐患。鉴于机场进近区是限制空域运行能力的主要瓶颈,针对如何提高空域资源利用率从而提升空域容量进行了进近区扇区规划,提出了考虑飞行流量、冲突发生的位置以及空域运行情况等因素建立的扇区容量均衡模型,利用霍夫曼编码原理进一步找到了扇区边界,并验证了方法的科学性和合理性。 相似文献
1000.
Stability and shape analysis of relative equilibrium for three-spacecraft electromagnetic formation 总被引:1,自引:0,他引:1
The invariant shapes for close formation flying with inter-craft electromagnetic force ensure several potential space applications. However, the 6-DOF relative equilibrium problem has not been systematically investigated. This paper mainly analyzes the invariant shapes of relative equilibrium for the three-spacecraft electromagnetic formation, and studies the families of invariant shape solutions with real and constant magnetic moments as well as their linear stability. The problem is examined based on the full nonlinear coupled dynamic models for collinear and general triangular configurations. The relative equilibrium conditions are analyzed to determine whether an invariant shape do exist, and the corresponding families of invariant shape solutions are identified for static and spinning configurations respectively. Finally, the linear stability of such invariant shapes is numerically discussed, which have shown that most invariant shapes are unstable and controllable. 相似文献