全文获取类型
收费全文 | 575篇 |
免费 | 187篇 |
国内免费 | 99篇 |
专业分类
航空 | 519篇 |
航天技术 | 156篇 |
综合类 | 61篇 |
航天 | 125篇 |
出版年
2024年 | 4篇 |
2023年 | 19篇 |
2022年 | 22篇 |
2021年 | 39篇 |
2020年 | 31篇 |
2019年 | 26篇 |
2018年 | 31篇 |
2017年 | 36篇 |
2016年 | 60篇 |
2015年 | 22篇 |
2014年 | 30篇 |
2013年 | 24篇 |
2012年 | 43篇 |
2011年 | 43篇 |
2010年 | 39篇 |
2009年 | 45篇 |
2008年 | 33篇 |
2007年 | 60篇 |
2006年 | 23篇 |
2005年 | 16篇 |
2004年 | 26篇 |
2003年 | 15篇 |
2002年 | 22篇 |
2001年 | 18篇 |
2000年 | 10篇 |
1999年 | 18篇 |
1998年 | 23篇 |
1997年 | 16篇 |
1996年 | 14篇 |
1995年 | 10篇 |
1994年 | 7篇 |
1993年 | 9篇 |
1992年 | 9篇 |
1991年 | 4篇 |
1990年 | 6篇 |
1989年 | 5篇 |
1988年 | 2篇 |
1987年 | 1篇 |
排序方式: 共有861条查询结果,搜索用时 124 毫秒
41.
42.
激光测高仪回波分解算法 总被引:1,自引:0,他引:1
开发了一种激光测高仪回波基本信息提取算法,对回波数据进行了高斯波分解,获取了高斯波分量的个数,及每个高斯波分量的波中心位置、宽度和幅度等参数.该算法首先根据回波拐点的数目和位置确定出高斯分量的个数及每个高斯分量的波中心位置和宽度初始值,随后利用线性最小二乘法计算出每个高斯分量的幅度,最后将经过选择和标记的高斯分量针对实际回波采用Levenberg-Marquardt方法进行拟合,得到优化后的高斯波基本参数.通过这些基本参数信息,能够进一步推导出激光测高仪光斑内各个反射表面的垂直分布、起伏程度和反射率等基本信息. 相似文献
43.
44.
45.
针对传统Allan方差法分析激光陀螺误差特性过程中,不能合理解释方差中部分噪声项出现负值的情况,而采用阻尼振荡的分析方法能够对此给出合理解释,却又损失了辨识精度的问题,提出了一种基于动态Allan方差法理论的改进Allan方差法。该方法将阻尼振荡模型与动态Allan方差模型相结合,使得辨识结果的分析过程更加合理。激光陀螺零偏误差的辨识与分析结果表明:改进Allan方差法的辨识结果精度略高些,在改进Allan方差的三维分析图中可以显示出零偏中存在的数据突变情况,能够反应激光陀螺误差的动态特性。因此,改进Allan方差法更适用于激光陀螺误差特性的分析。 相似文献
46.
AZ31镁合金板热成形中的屈服和损伤:本构实现与数值分析 总被引:1,自引:1,他引:0
为了准确预测各向异性镁合金板的成形质量,将改进的GTN损伤模型与各向异性拉压不对称的CPB06屈服本构耦合,并考虑了屈服面形状随塑性应变累积的变化,得到了考虑本构参数随塑性应变演化的各向异性屈服CPB06-GTN损伤模型。基于该模型,在ABAQUS/Explict中编译得到了相应的VUMAT子程序,采用单个单元进行了单轴拉伸和压缩模拟,并通过与实验一致性对比验证了子程序的正确性。使用子程序不仅能够模拟镁合金的各向异性屈服及其不规则的硬化,同时也能够模拟镁合金的损伤破坏。此外,采用编写的子程序进行了热拉深成形的数值模拟,模拟预测与实验结果对比表明,采用各向异性损伤模型的计算结果能够准确预测镁合金的变形及其损伤破坏,模拟结果与实验数据吻合;采用合适的压边力和成形的温度条件及非等温成形方法能够提高镁合金的成形性。 相似文献
47.
《中国航空学报》2021,34(2):104-123
Plastic forming is one of enabling and fundamental technologies in advanced manufacturing chains. Design optimization is a critical way to improve the performance of the forming system, exploit the advantages of high productivity, high product quality, low production cost and short time to market and develop precise, accurate, green, and intelligent (smart) plastic forming technology. However, plastic forming is quite complicated, relating to multi-physics field coupling, multi-factor influence, multi-defect constraint, and triple nonlinear, etc., and the design optimization for plastic forming involves multi-objective, multi-parameter, multi-constraint, nonlinear, high-dimensionality, non-continuity, time-varying, and uncertainty, etc. Therefore, how to achieve accurate and efficient design optimization of products, equipment, tools/dies, and processing as well as materials characterization has always been the research frontier and focus in the field of engineering and manufacturing. In recent years, with the rapid development of computing science, data science and internet of things (IoT), the theories and technologies of design optimization have attracted more and more attention, and developed rapidly in forming process. Accordingly, this paper first introduced the framework of design optimization for plastic forming. Then, focusing on the key problems of design optimization, such as numerical model and optimization algorithm, this paper summarized the research progress on the development and application of the theories and technologies about design optimization in forming process, including deterministic and uncertain optimization. Moreover, the applicability of various modeling methods and optimization algorithms was elaborated in solving the design optimization problems of plastic forming. Finally, considering the development trends of forming technology, this paper discusses some challenges of design optimization that may need to be solved and faced in forming process. 相似文献
48.
49.
50.
Removing orbital debris with lasers 总被引:2,自引:0,他引:2
Claude R. Phipps Kevin L. Baker Stephen B. Libby Duane A. Liedahl Scot S. Olivier Lyn D. Pleasance Alexander Rubenchik James E. Trebes E. Victor George Bogdan Marcovici James P. Reilly Michael T. Valley 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
Orbital debris in low Earth orbit (LEO) are now sufficiently dense that the use of LEO space is threatened by runaway collision cascading. A problem predicted more than thirty years ago, the threat from debris larger than about 1 cm demands serious attention. A promising proposed solution uses a high power pulsed laser system on the Earth to make plasma jets on the objects, slowing them slightly, and causing them to re-enter and burn up in the atmosphere. In this paper, we reassess this approach in light of recent advances in low-cost, light-weight modular design for large mirrors, calculations of laser-induced orbit changes and in design of repetitive, multi-kilojoules lasers, that build on inertial fusion research. These advances now suggest that laser orbital debris removal (LODR) is the most cost-effective way to mitigate the debris problem. No other solutions have been proposed that address the whole problem of large and small debris. A LODR system will have multiple uses beyond debris removal. International cooperation will be essential for building and operating such a system. 相似文献