全文获取类型
收费全文 | 313篇 |
免费 | 60篇 |
国内免费 | 50篇 |
专业分类
航空 | 212篇 |
航天技术 | 93篇 |
综合类 | 24篇 |
航天 | 94篇 |
出版年
2023年 | 11篇 |
2022年 | 11篇 |
2021年 | 9篇 |
2020年 | 14篇 |
2019年 | 22篇 |
2018年 | 9篇 |
2017年 | 22篇 |
2016年 | 13篇 |
2015年 | 17篇 |
2014年 | 21篇 |
2013年 | 15篇 |
2012年 | 22篇 |
2011年 | 33篇 |
2010年 | 23篇 |
2009年 | 15篇 |
2008年 | 18篇 |
2007年 | 21篇 |
2006年 | 18篇 |
2005年 | 21篇 |
2004年 | 10篇 |
2003年 | 11篇 |
2002年 | 7篇 |
2001年 | 11篇 |
2000年 | 7篇 |
1999年 | 5篇 |
1998年 | 5篇 |
1997年 | 3篇 |
1996年 | 5篇 |
1995年 | 4篇 |
1994年 | 4篇 |
1993年 | 3篇 |
1992年 | 2篇 |
1991年 | 3篇 |
1990年 | 3篇 |
1989年 | 2篇 |
1988年 | 2篇 |
1986年 | 1篇 |
排序方式: 共有423条查询结果,搜索用时 15 毫秒
81.
武丁二 《中国民航学院学报》2009,27(2):36-37
通过对LD端泵Nd:YVO4固体激光器输出特性的研究,并运用传播圆和变换圆理论的分析,得出了晶体双折射是影响激光器输出特性重要因素,并与实验相吻合。 相似文献
82.
Songtao Han Axel Nothnagel Zhongkai Zhang Rüdiger Haas Qiang Zhang 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(5):1754-1767
Extracting the group and phase delays of interferometric observations produced in the Very Long Baseline Interferometry (VLBI) measurement concept requires a special fringe fitting and delay search algorithm for the recorded bandwidth. While fringe fitting is in use routinely for several megahertz wide channels in geodetic and astrometric VLBI with quasar observations, fringe fitting for artificial tones of very small bandwidth of artificial signals for Differential One-way Ranging (DOR) requires a different way of handling. In a project called Observing the Chang’E-3 Lander with VLBI (OCEL), the DOR tones emitted by the Chang’E-3 lander were observed in a standard geodetic VLBI mode with 8 or 4?MHz wide channels to maintain compatibility with the corresponding quasar observations. For these observations, we modified the existing fringe fitting program of the Haystack Observatory Processing Software (HOPS), fourfit, to properly handle narrow band DOR tones. The main motivations are that through this modification, the data of quasars and artificial radio sources can be processed in the existing geodetic analysis pipeline, and that the algorithm can be used for similar projects as well. In this paper, we describe the algorithm and show that the new algorithm produces much more reliable group delay results than using the standard fourfit algorithm. This is done by a simulation test and in particular by processing of real observations. It is shown that in many cases, systematic deviations of several nanoseconds, which are seen with the standard fourfit algorithm, can be avoided. The ultimate benefit of the new procedure is demonstrated by reducing the errors in delay triangle closures by at least a factor of 3, which, in the OCEL case, is from ~300 to ~100?ps. 相似文献
83.
We investigate the relation between nontrivial spatial concepts such as holes and string loops from a qualitative spatial reasoning perspective. In particular, we concentrate on a family of puzzles dealing with this kind of objects and explain how a loop formed in a string shows a similar behavior to a hole in an object, at least regarding the qualitative constraints it imposes on the solution of the puzzle. Unlike regular holes, however, we describe how string loops can be dynamically created and destroyed depending on the actions on the string. Furthermore, under a Knowledge Representation point of view, we provide a formalization that allows the different puzzle states to be described in terms of string crossings and loops, together with the actions that can be executed for a state transition and the complex effects they cause on the state representation. This implies the consideration of a formal representation of the side effects of actions that create or destroy string loops and the soundness of this representation with respect to the more general representation of string states in knot theory. 相似文献
84.
郝其祥 《中国民航学院学报》1998,16(6):15-17
介绍了转折圆的运动学特性,论述了求铰链四杆机构的转折圆,以及利用转折圆进行铰链四杆机构近似直线导向设计的方法。 相似文献
85.
86.
87.
编队卫星空间状态参数估计量对ATI测速精度影响 总被引:1,自引:0,他引:1
基于对影响沿航向干涉(ATI)测速精度的特征量分析,建立了卫星空间状态参数估计量与ATI测速精度特征量,特征量与测速的关联数学模型。仿真给出了不同场景设置下的特征量精度、误差传播矩阵和测量误差传递关系的精度影响因子,以及最终空间状态参数估计量对测速精度的影响。 相似文献
88.
89.
To improve the computational efficiency and hold calculation accuracy at the same time,we study the parallel computation for radiation heat transfer. In this paper, the discrete ordinates method(DOM) and the spatial domain decomposition parallelization(DDP) are combined by message passing interface(MPI) language. The DDP–DOM computation of the radiation heat transfer within the rectangular furnace is described. When the result of DDP–DOM along one-dimensional direction is compared with that along multi-dimensional directions, it is found that the result of the latter one has higher precision without considering the medium scattering. Meanwhile, an in-depth study of the convergence of DDP–DOM for radiation heat transfer is made. Analyzing the cause of the weak convergence, we relate the total number of iteration steps when the convergence is obtained to the number of sub-domains. When we decompose the spatial domain along one-,two- and three-dimensional directions, different linear relationships between the number of total iteration steps and the number of sub-domains will be possessed separately, then several equations are developed to show the relationships. Using the equations, some phenomena in DDP–DOM can be made clear easily. At the same time, the correctness of the equations is verified. 相似文献
90.
针对多臂航天器在轨操控过程中可能存在的多链、闭环、环链混合等多种拓扑构型及相应的动力学模型变化,提出基于空间算子代数理论(SOA)的高效统一动力学建模方法。首先,提出了描述多臂航天器部件连接关系的构型参数,并基于构型参数提出了多臂航天器拓扑构型描述矩阵的自主生成方法。其次,基于空间算子代数理论,将通路矩阵与空间转移算子相结合,提出了变拓扑多臂航天器统一动力学建模方法。最后,将数值仿真结果与多体动力学仿真软件的仿真结果进行比对,验证所提方法的有效性。仿真结果表明,对于不同的拓扑结构,所提出的O(n)阶统一动力学建模方法能准确描述变拓扑情况下的多臂航天器动力学响应。 相似文献