全文获取类型
收费全文 | 274篇 |
免费 | 85篇 |
国内免费 | 64篇 |
专业分类
航空 | 216篇 |
航天技术 | 63篇 |
综合类 | 34篇 |
航天 | 110篇 |
出版年
2024年 | 2篇 |
2023年 | 4篇 |
2022年 | 17篇 |
2021年 | 20篇 |
2020年 | 17篇 |
2019年 | 9篇 |
2018年 | 14篇 |
2017年 | 20篇 |
2016年 | 14篇 |
2015年 | 12篇 |
2014年 | 13篇 |
2013年 | 19篇 |
2012年 | 28篇 |
2011年 | 23篇 |
2010年 | 17篇 |
2009年 | 12篇 |
2008年 | 18篇 |
2007年 | 19篇 |
2006年 | 17篇 |
2005年 | 13篇 |
2004年 | 11篇 |
2003年 | 18篇 |
2002年 | 16篇 |
2001年 | 8篇 |
2000年 | 11篇 |
1999年 | 15篇 |
1998年 | 5篇 |
1997年 | 6篇 |
1996年 | 1篇 |
1995年 | 5篇 |
1994年 | 5篇 |
1993年 | 4篇 |
1992年 | 3篇 |
1991年 | 1篇 |
1990年 | 2篇 |
1988年 | 2篇 |
1986年 | 2篇 |
排序方式: 共有423条查询结果,搜索用时 656 毫秒
41.
Zong He 《中国航天(英文版)》2010,(1)
<正>The Chinese government has consistently regarded the space industry as an integral part of the state's comprehensive development strategy,and upheld that the exploration and utilization of outer space should be for peaceful purposes and to benefit the whole of mankind.China's space activities fall into three categories: space technology,space applications and space science.China has made the following progress in these three areas during 2009. 相似文献
42.
Optimal guidance for reentry vehicles based on indirect Legendre pseudospectral method 总被引:2,自引:0,他引:2
Development of a feasible guidance scheme for reentry vehicles is a challenge because of its significant nonlinearity and multi-constraints. A method for the implementation of three-degree-of-freedom guidance for constrained reentry vehicle is presented in the paper. First, the constrained trajectory is generated by Legendre pseudospectral method (LPM) and then the feasibily of the trajectory is validated. Based on the obtained reference trajectory, the guidance problem is converted into a trajectory state regulation problem which is a linear time varying system. A robust state feedback guidance law is generated in real time using indirect Legendre pseudospectral feedback method. Finally, simulation results illustrate that the overall guidance scheme can lead to a very accurately controlled flight with all the constraints satisfied even in the presence of initial state uncertainty. 相似文献
43.
Zong He 《中国航天(英文版)》2010,(2)
<正>On April 24,1970,China successfully launched its first man-made satellite,DFH-1. It was a milestone in China's space history,making China the 5th country capable of independently developing, launching and operating satellites following the former Soviet Union, the United States,France and Japan. Since then China's satellites have been launched into space one after another and benefit mankind due to their advantages. Over the past 40 years,China has 相似文献
44.
Zong He 《中国航天(英文版)》2013,(2):19-20
On April 15,2013,the central committee of CPC and the State Council of China decided to establish a Board of Executives for China Aerospace Science and Technology(CASC)and Mr.Xu Dazhe was appointed Chairman of CASC 相似文献
46.
47.
微絮凝变孔隙深层过滤处理低浊度废水研究 总被引:1,自引:0,他引:1
本文研究了微絮凝变孔隙深层过滤处理低浊度废水时,滤料粒径、絮凝剂种类、投加量、滤速等因素对过滤效果的影响。试验结果表明:在达到相同出水水质的情况下,由于变孔隙结构等原因,该系统具有用药量省、阻力损失小、出水量大及整床过滤效能好等优点。 相似文献
48.
TA17钛合金是航空航天等工程中重要的结构材料,其疲劳裂纹扩展性能直接影响整体结构的安全性和完整性。本文基于Cr2Ni2MoV钢材紧凑拉伸试样斜裂纹疲劳裂纹扩展的试验结果,验证了ABAQUS软件XFEM模块用于分析平面应力状态下疲劳裂纹扩展的有效性,然后采用XFEM模块分析了TA17钛合金及其连接件的疲劳裂纹扩展性能。结果表明降低最大荷载、减小加载比和采用长圆孔型均可有效提高TA17钛合金连接件的疲劳寿命。采用XFEM模块可以预测连接件疲劳寿命的S-N曲线,预测TA17钛合金结构载荷增大33.3%,疲劳寿命减小为原来的1/4,可为工程疲劳设计提供参考依据。 相似文献
49.
In this paper, we present a distributed framework for the lidar-based relative state estimator which achieves highly accurate, real-time trajectory estimation of multiple Unmanned Aerial Vehicles(UAVs) in GPS-denied environments. The system builds atop a factor graph, and only onboard sensors and computing power are utilized. Benefiting from the keyframe strategy, each UAV performs relative state estimation individually and broadcasts very partial information without exchanging raw data. The com... 相似文献
50.