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   545篇
  免费   66篇
  国内免费   70篇
航空   296篇
航天技术   212篇
综合类   36篇
航天   137篇
  2023年   4篇
  2022年   7篇
  2021年   16篇
  2020年   9篇
  2019年   11篇
  2018年   14篇
  2017年   12篇
  2016年   16篇
  2015年   9篇
  2014年   21篇
  2013年   32篇
  2012年   35篇
  2011年   33篇
  2010年   33篇
  2009年   29篇
  2008年   36篇
  2007年   25篇
  2006年   33篇
  2005年   35篇
  2004年   24篇
  2003年   22篇
  2002年   18篇
  2001年   17篇
  2000年   13篇
  1999年   6篇
  1998年   14篇
  1997年   7篇
  1996年   7篇
  1995年   14篇
  1994年   8篇
  1993年   6篇
  1992年   15篇
  1991年   4篇
  1990年   4篇
  1989年   8篇
  1988年   4篇
  1987年   7篇
  1986年   3篇
  1985年   8篇
  1984年   12篇
  1983年   9篇
  1982年   9篇
  1981年   14篇
  1980年   2篇
  1972年   2篇
  1971年   4篇
  1970年   2篇
  1969年   2篇
  1968年   1篇
  1967年   1篇
排序方式: 共有681条查询结果,搜索用时 15 毫秒
101.
Cylindrical heterogeneous detonation waves   总被引:1,自引:0,他引:1  
Further experimental studies of blast wave initiated cylindrical heterogeneous (liquid fuel drops, gas oxidizer) detonation waves are described. A pie-shaped shock tube, used for these studies, was altered in certain ways so as to improve the modeling of cylindrical waves. These modifications, along with some operational aspects, are briefly discussed. The breech of the facility, where the blast wave is generated by an explosive, became distorted with usage. Results are presented which show that lower detonation velocities are realized with the damaged breech (other conditions being the same). A photographic and pressure switch wave time of arrival study was made to ascertain the wave shape. Photographs are shown which show that the waves, blast as well as detonation, are close to cylindrical. However, in some cases there is appreciable distortion of the wave front by debris ahead of the wave. Presumably this debris comes from the blasting cap used to ignite the condensed explosive. A series of experiments was conducted using kerosene drops of 388 μm diameter dispersed in air through use of a large number of hypodermic needles. Radial fuel void regions were established by cutting off the fuel flow to a number of needles. Preliminary results relating to the effect of the size of the cloud gap on detonation velocity, quenching, and the initiator energy levels required for detonation are discussed.  相似文献   
102.
The early evolution of a photocatalytic system of the porphyrin type, able to efficiently collect and utilize solar energy for primary electron transfer is discussed. Experimental results concerning some spectral and photochemical properties of the porphyrins, biosynthetic precursors of chlorophyll and their complexes with polymeric templates are reviewed. Protoporphyrin IX associated with pigmented proteinoid is demonstrated to be a favourable candidate for a role of a photosensitizer of the first photosynthetic reaction centers. The origin and early evolution of the photosynthetic electron transfer chain and of the phosphorylating mechanism are discussed with emphasis on the energetic mechanisms of archaebacteria.  相似文献   
103.
针对目前通信辐射源个体识别算法在实际试验中由于各类干扰信号和多径衰落导致识别率较低的问题,提出一种用于识别算法前端的信号分离算法,可有效地减少其他电磁信号对于识别算法输入信号的影响,从而提高在复杂电磁环境中通信辐射源个体识别的正确识别率。该算法将灾变策略和搜索状态的自适应引入量子粒子群算法,通过对混合信号的联合对角化从截获的观测信号中提取出目标通信辐射源的有用信号。为了更加系统、直观地衡量算法的分离效果,提出分离熵来量化算法的整体性能。仿真结果表明,该分离算法可以把目标通信辐射源的有用信号从复杂电磁环境中提取出来,从而提高通信辐射源个体识别在复杂电磁环境中的正确识别率,具有较好的可行性和有效性。  相似文献   
104.
空间科学任务协同设计论证存在设计方案耦合强,数据一致性差,数据变更难,数据与流程脱节等问题.为了解决上述问题,建立了典型空间科学任务的多层数字化模型;采用图形化方式对论证流程进行建模,并建立流程与数据的映射关系;通过共享数据池的方式为多岗位用户提供多方案数据协同机制;采用消息总线对数据变更进行及时提醒;利用方案依赖关系矩阵来判别方案耦合关系,最终自动合并任务总体设计方案.作为一个分布式平台,空间科学任务协同设计平台采用Eclipse RCP和Spring技术架构,整合了Hibernate、工作流Activiti5等中间件,提供统一门户,支持多岗位、多任务、多方案、多版本的管理能力,提供论证流程监控、数据协同交互等功能.结合某空间科学任务论证验证了该平台的有效性.   相似文献   
105.
The retrieval of a tethered satellite system is intrinsically unstable. This paper develops a new control strategy to retrieve the tethered satellite system stably and quickly using the fractional order control theory. The governing equation of the tethered satellite system and classic linear feedback tension control law were first reviewed and examined as a benchmark. Then, a new fractional order tension control law has been to avoid the tethered satellite winds around the main satellite near the end of retrieval by existing integer order tension control laws. The newly proposed control law has been discretized and implemented by the Laplace transform and Tustin operator. Unlike the existing integer order control laws, which are based on the feedback of current state and memoryless, the fractional order control law has the memory of previous states and thus controls the tether retrieval more smoothly while maintaining the retrieving speed. The effectiveness and advantage of the new fractional order tension control law is demonstrated numerically by comparing with its integer order counterpart. The results show that the new control law not only retrieves the subsatellite without winding around the main satellite, but also provides a better control performance with smaller in-plane libration angles.  相似文献   
106.
针对飞航导弹单独使用时SINS存在姿态估计精度随时间降低的问题,提出了基于未知地标被动观测的SINS俯仰姿态误差估计方法。首先,根据飞航导弹中制导段飞行的特点,把SINS俯仰姿态误差估计问题转化为攻角估计问题。然后,在不改变导弹巡航路径的前提下,利用弹上成像导引头对视场内任意未知地标连续被动观测,分别提出了弹体坐标系和速度坐标系下的攻角估计方法,并分析了观测噪声对量测方程系数的影响。最后,利用平均去噪的思想对估计结果进行处理,提高了SINS俯仰姿态误差的估计精度。仿真结果表明:两种方法都能有效估计出飞航导弹SINS俯仰姿态量测误差。  相似文献   
107.
Oehler DZ  Allen CC 《Astrobiology》2012,12(6):601-615
This paper presents the hypothesis that the well-known giant polygons and bright mounds of the martian lowlands may be related to a common process-a process of fluid expulsion that results from burial of fine-grained sediments beneath a body of water. Specifically, we hypothesize that giant polygons and mounds in Chryse and Acidalia Planitiae are analogous to kilometer-scale polygons and mud volcanoes in terrestrial, marine basins and that the co-occurrence of masses of these features in Chryse and Acidalia may be the signature of sedimentary processes in an ancient martian ocean. We base this hypothesis on recent data from both Earth and Mars. On Earth, 3-D seismic data illustrate kilometer-scale polygons that may be analogous to the giant polygons on Mars. The terrestrial polygons form in fine-grained sediments that have been deposited and buried in passive-margin, marine settings. These polygons are thought to result from compaction/dewatering, and they are commonly associated with fluid expulsion features, such as mud volcanoes. On Mars, in Chryse and Acidalia Planitiae, orbital data demonstrate that giant polygons and mounds have overlapping spatial distributions. There, each set of features occurs within a geological setting that is seemingly analogous to that of the terrestrial, kilometer-scale polygons (broad basin of deposition, predicted fine-grained sediments, and lack of significant horizontal stress). Regionally, the martian polygons and mounds both show a correlation to elevation, as if their formation were related to past water levels. Although these observations are based on older data with incomplete coverage, a similar correlation to elevation has been established in one local area studied in detail with newer higher-resolution data. Further mapping with the latest data sets should more clearly elucidate the relationship(s) of the polygons and mounds to elevation over the entire Chryse-Acidalia region and thereby provide more insight into this hypothesis.  相似文献   
108.
提出一种具有容错能力的进化数据流聚类算法FTGDStream (Fault-Tolerant Grid-Density Clustering over Data Stream),通过在聚类过程中引入适当的松弛条件,从而在含有噪声的真实世界数据中获取更加泛化的有用知识.首先利用基于相似性度量和小波技术的HLSFTS (Hierarchical Lifting Scheme Fault-Tolerant Synopses)层次概要数据结构实现在线微聚类过程,然后采用基于网格密度的聚类算法实现离线宏聚类过程.在线算法所构造的小波概要数据结构对原始数据的高压缩率降低了离线网格密度聚类算法的计算负载,提高了二层数据流聚类算法的效率.在UCI数据集上的仿真实验结果表明,FTGDStream算法可以聚类任意空间形状的数据并且适用于高维数据流环境,是一种具有容错能力的高效数据流聚类算法.  相似文献   
109.
魏东  杜雁霞  石友安  桂业伟 《宇航学报》2015,36(10):1108-1113
为获得非均匀气动加热条件下高超声速飞行器不同部位的合适的热防护系统厚度,发展了一种基于网格变形技术(ASD)的隔热层结构优化方法。以高超声速飞行器的复合材料隔热层结构为研究对象,采用有限元法在局部均布热流载荷、三角形均变热流载荷和二次函数热流载荷等作用条件下建立隔热层结构的热固耦合分析模型,提出了基于ASD技术与热固耦合分析相结合的结构轻量化设计方法。结果表明,基于网格变形技术能够快速有效地解决优化过程中的网格自动更新问题,并得到了光滑柔顺的厚度形状曲线,优化后更充分发挥了隔热层结构各层材料的承载能力。  相似文献   
110.
载人飞船飞行任务中搭载的有效载荷设备质量、体积大并且安装要求苛刻,而返回舱内空间狭小且舱内环境复杂。针对这个问题,文章提出了通过改装返回舱座椅作为有效载荷搭载安放的方案。经过试验验证表明,该方案对飞船的影响很小,并且满足有效载荷设备搭载要求。  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