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   5408篇
  免费   844篇
  国内免费   677篇
航空   3744篇
航天技术   1050篇
综合类   746篇
航天   1389篇
  2024年   32篇
  2023年   130篇
  2022年   171篇
  2021年   222篇
  2020年   226篇
  2019年   232篇
  2018年   213篇
  2017年   223篇
  2016年   264篇
  2015年   234篇
  2014年   436篇
  2013年   327篇
  2012年   382篇
  2011年   443篇
  2010年   278篇
  2009年   292篇
  2008年   359篇
  2007年   389篇
  2006年   327篇
  2005年   311篇
  2004年   245篇
  2003年   217篇
  2002年   157篇
  2001年   143篇
  2000年   94篇
  1999年   90篇
  1998年   91篇
  1997年   53篇
  1996年   37篇
  1995年   45篇
  1994年   37篇
  1993年   50篇
  1992年   44篇
  1991年   42篇
  1990年   34篇
  1989年   29篇
  1988年   18篇
  1987年   3篇
  1986年   1篇
  1984年   8篇
排序方式: 共有6929条查询结果,搜索用时 359 毫秒
841.
基于软件工程思想方法的CAI课件开发   总被引:4,自引:0,他引:4  
介绍了软件工程思想方法,运用软件工程思想方法基于瀑布模型分析了CAI课件开发过程,实践创作开发了基于Web的多媒体《概率论与数理统计》CAI课件。  相似文献   
842.
Multirotor has been applied to many military and civilian mission scenarios. From the perspective of reliability, it is difficult to ensure that multirotors do not generate hardware and software failures or performance anomalies during the flight process. These failures and anomalies may result in mission interruptions, crashes, and even threats to the lives and property of human beings. Thus, the study of flight reliability problems of multirotors is conductive to the development of the drone industry and has theoretical significance and engineering value. This paper proposes a reliable flight performance assessment method of multirotors based on an Interacting Multiple Model Particle Filter (IMMPF) algorithm and health degree as the performance indicator. First, the multirotor is modeled by the Stochastic Hybrid System (SHS) model, and the problem of reliable flight performance assessment is formulated. In order to solve the problem, the IMMPF algorithm is presented to estimate the real-time probability distribution of hybrid state of the established SHS-based multirotor model, since it can decrease estimation errors compared with the standard interacting multiple model algorithm based on extended Kalman filter. Then, the reliable flight performance is assessed with health degree based on the estimation result. Finally, a case study of a multirotor suffering from sensor anomalies is presented to validate the effectiveness of the proposed method.  相似文献   
843.
航天测控装备跟踪质量考核标准分析   总被引:1,自引:0,他引:1  
针对航天测控装备在役考核标准缺乏的问题,分析了航天测控(Space tracking telemetry and control,TTC)标准的现状,梳理了可用于在役考核的现有航天装备相关标准。提出了航天测控装备考核跟踪质量稳定性的参考标准,分析了标准对在役考核要求的适用性,并对跟踪质量稳定性考核科目进行了修正扩展。实际工程算例表明考核效果合理有效,跟踪质量稳定性考核标准可为在役考核标准制定提供借鉴参考。  相似文献   
844.
指出了我国航天器名的英译用汉语拼音的不足;建议我国航天器的英译名以意译为主,音译为辅;提出了航天器名意译的原则和我国全部航天器按意译的英语名建议。  相似文献   
845.
Future piloted missions to explore asteroids, Mars, and other targets beyond the Moon will experience strict limitations on communication between vehicles in space and control centers on Earth. These limitations will require crews to operate with greater autonomy than any past space mission has demonstrated. The Antarctic Search for Meteorites (ANSMET) project, which regularly sends small teams of researchers to remote parts of the southern continent, resembles a space mission in many ways but does not rely upon a control center. It provides a useful crew autonomy model for planners of future deep space exploration missions. In contrast to current space missions, ANSMET gives the crew the authority to adjust competing work priorities, task assignments, and daily schedules; allows the crew to be the primary monitor of mission progress; demands greater crew accountability for operational errors; requires the crew to make the most of limited communication bandwidth; adopts systems designed for simple operation and failure recovery; and grants the crew a leading role in the selection and stowage of their equipment.  相似文献   
846.
为了使新疆和田地区夏季在经济性合理前提下使室内通风环境满足人体热舒适要求。利用蒸发冷却技术将室外空气处理后送入室内,通过数值模拟分析得出在夏季室内负荷最大时刻采用机械辅助式自然通风,使得室温能够雏持在26-8℃,风速为0.6m/s,基本满足人体热舒适要求。在室外温度适宜的过渡季节采用Trombe墙和太阳能烟囱复合的自然通风系统,建筑太阳能烟囱的经济高度为10m。  相似文献   
847.
圆球绕流场的尾涡分析和升阻力研究   总被引:5,自引:0,他引:5  
采用自编的分块算法程序模拟了雷诺数在20~1000之间的圆球绕流场.在Re=25时捕捉到流动分离,与试验结果一致.对Re=250时稳态非对称尾流区内流体的输运情况进行研究,证实圆球绕流场中纵向对称面的存在.对于非稳态流动,主要研究了阻力和横向力的时间变化规律,并分析了频谱特征.计算发现横向合力主要在横截面上两个很窄的区间内偏移.经过几种不同涡定义方法的优劣测试,本文采用Hunt等人介绍的Q-定义方法对非稳态绕流场的尾涡结构进行了直观描述.  相似文献   
848.
The space science research has been started in Egypt since 1910 by measuring the solar constant as indication of solar radiation at Helwan Observatory. The solar sunspot studies and its influence on the Nile flooding was erected and operated at Helwan as a first solar station in Egypt during 1957. Zeiss-Coude’ refractor was installed in 1964. Astronomy and space science educations started in Egypt at the university level since 1936 at Department of Astronomy and Meteorology of Cairo University. Undergraduate and graduate education in Egypt will be discussed in this work.  相似文献   
849.
Microsoft Access 2000数据库作为常用的桌面数据库软件,在中小型的数据库系统中得到了广泛的应用。针对Access2000安全性能不高,探讨如何设置及提高Access2000的安全性方法。  相似文献   
850.
While adopting an elevation-over-azimuth architecture by an inter-satellite linkage antenna of a user satellite, a zenith pass problem always occurs when the antenna is tracing the tracking and data relay satellite (TDRS). This paper deals with this problem by way of, firstly, introducing movement laws of the inter-satellite linkage to predict the movement of the user satellite antenna followed by analyzing the potential pass moment and the actual one of the zenith pass in detail. A number of specific orbit altitudes for the user satellite that can remove the blindness zone are obtained. Finally, on the base of the predicted results from the movement laws of the inter-satellite linkage, the zenith pass tracing strategies for the user satellite antenna are designed under the program guidance using a trajectory preprocessor. Simulations have confirmed the reasonability and feasibility of the strategies in dealing with the zenith pass problem.  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