全文获取类型
收费全文 | 207篇 |
免费 | 46篇 |
国内免费 | 52篇 |
专业分类
航空 | 186篇 |
航天技术 | 62篇 |
综合类 | 23篇 |
航天 | 34篇 |
出版年
2024年 | 3篇 |
2023年 | 7篇 |
2022年 | 9篇 |
2021年 | 26篇 |
2020年 | 16篇 |
2019年 | 13篇 |
2018年 | 12篇 |
2017年 | 11篇 |
2016年 | 11篇 |
2015年 | 9篇 |
2014年 | 22篇 |
2013年 | 16篇 |
2012年 | 13篇 |
2011年 | 13篇 |
2010年 | 9篇 |
2009年 | 9篇 |
2008年 | 13篇 |
2007年 | 22篇 |
2006年 | 9篇 |
2005年 | 8篇 |
2004年 | 7篇 |
2003年 | 4篇 |
2002年 | 6篇 |
2001年 | 6篇 |
2000年 | 3篇 |
1999年 | 4篇 |
1998年 | 8篇 |
1997年 | 2篇 |
1995年 | 3篇 |
1993年 | 6篇 |
1990年 | 1篇 |
1984年 | 4篇 |
排序方式: 共有305条查询结果,搜索用时 20 毫秒
231.
在室温下以等径弯曲通道变形(ECAP)技术制备超细晶工业纯钛,利用光学显微镜(OM)和透射电子显微镜(TEM)研究室温ECAP变形纯钛微观组织演变过程,并讨论纯钛室温ECAP变形的显微组织演化机制。结果表明:显微组织演化分为3个不同阶段,分别对应3种不同机制:第一阶段在真应变ε≤1.27时,为位错滑移和孪生交互作用细化机制,形成含有高密度位错和孪晶的板条状组织;第二阶段在真应变量1.27<ε<2.54时,为动态回复细化机制,晶粒进一步细化至~0.25μm,形成典型的变形亚晶组织;第三阶段在真应变量ε≥2.54时,为不平衡晶界的转动细化机制,形成平均晶粒尺寸约为0.2μm的等轴状大角度晶界超细晶组织。 相似文献
232.
233.
丁汀 《民用飞机设计与研究》2012,(2):44-48,66
放眼全球化的当今社会,航空交通密度日益增大,机场运营繁忙,部分枢纽型机场的吞吐量逐渐趋近饱和。这种现状对先进的机场场面导向和控制系统提出了更高的要求。与传统的机场导向和控制系统SMGCS(Surface Movement Guidance and Control System)相比,先进的机场场面导向和控制系统A-SMGCS(Advanced-Surface Movement Guidance and Control System)功能分为四部分:监视、路由、导向及控制。将对A-SMGCS的应用背景和发展状况给出较为全面的调研总结[1],并结合ICAOA-SMGCS Manual[3]论述对A-SMGCS提出详细功能需求,最后在此基础上提出A-SMGCS的系统功能架构。 相似文献
234.
降雨作为一种气象条件,与飞机尾涡相互作用,改变自身与尾涡的动力学特性.高强度的尾涡导致后机难以着陆、复飞甚至坠机等后果,因此尾涡的演化进程对评估后机的飞行安全有重要意义.为了分析尾涡与降雨的相互干扰,基于欧拉-欧拉多相流模型,研究了降雨条件下的尾涡演化特性.对于多相流模型中的空气相模拟,采用大涡模拟湍流模型,雨相通过两... 相似文献
235.
采用主流FPGA的数字电路在线生长进化方法 总被引:1,自引:0,他引:1
采用主流FPGA器件构建了在线进化平台,提出了一种适合较大规模数字电路在线进化的生长进化方法。该方法模拟植物生长机理进化以解决进化速度缓慢问题,采用增长验证评估方法取代传统的穷举式验证评估方法来解决在线验证评估难题;应用免疫遗传算法克服遗传算法的早熟收敛问题;采用多参数级联十进制整数编码方法缩短染色体长度;采用生长进化方法成功地进化出了16位加法器和8位乘法器。对比实验结果表明,采用生长进化方法无论是进化出的电路规模,还是进化速度均优于传统的直接进化方法。 相似文献
236.
P. Mazzei A. Marino R. Rampazzo G. Galletta D. Bettoni 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
We are investigating the co-evolution of galaxies within groups combining multi-wavelength photometric and 2D kinematical observations. Here we focus on S0s showing star formation in ring/arm-like structures. We use smooth particle hydrodynamical simulations (SPH) with chemo-photometric implementation which provide dynamical and morphological information together with the spectral energy distribution (SED) at each evolutionary stage. As test cases, we simulate the evolution of two such S0s: NGC 1533 and NGC 3626. 相似文献
237.
A. Marino L. Bianchi P. Mazzei R. Rampazzo G. Galletta 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
With the aim of investigating galaxy evolution in nearby galaxy groups, we analyzed the spectral energy distribution of 24 galaxies, members of two groups in the Leo cloud, USGC U268 and USGC U376. We estimated the ages and stellar masses of the galaxies by fitting their total apparent magnitudes from far-ultraviolet to near-infrared with population synthesis models. The comparison of the results for a subsample of galaxies with smooth particle hydrodynamic (SPH) simulations with chemo-photometric implementation, shows that in most cases the estimated stellar masses obtained with the two different approaches are in good agreement. The kinematical and dynamical analysis indicates that USGC U268 is in a pre-virial collapse phase while USGC U376 is likely in a more evolved phase towards virialization. 相似文献
238.
Qi Liu Shuangcheng Zhang 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(3):975-984
This paper presents an improved new method with differential evolution and the cubic spline approach is proposed to retrieve sea level height based on GNSS SNR observations from a single geodetic receiver. Considering the B-spline function is unstable at the beginning or end, and the feature that B-spline functions do not pass through nodes may introduce errors. Thus, the cubic spline is applied to the retrieval process and accounts for a continuous and smooth in sea level retrieval time series. Besides, the biases caused by tropospheric delay and dynamic sea level are considered and corrected. Testing data from two stations with different tidal range and the final solution agrees well with measurements from co-located tide gauges, reaching the RMSE of 3.67 cm at Friday Harbor, Washington, and 1.36 cm at Onsala, Sweden. Comparison of the nonlinear least squares, this method leads to a clear increase in precision of the sea level retrievals within 50%. Additionally, referring to the result of Purnell et al. (2020) and the IAG inter-comparison campaign, the results of this paper show more potential. 相似文献
239.
Mingming Wang Jianjun Luo Jing Fang Jianping Yuan 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(6):1525-1536
The existence of the path dependent dynamic singularities limits the volume of available workspace of free-floating space robot and induces enormous joint velocities when such singularities are met. In order to overcome this demerit, this paper presents an optimal joint trajectory planning method using forward kinematics equations of free-floating space robot, while joint motion laws are delineated with application of the concept of reaction null-space. Bézier curve, in conjunction with the null-space column vectors, are applied to describe the joint trajectories. Considering the forward kinematics equations of the free-floating space robot, the trajectory planning issue is consequently transferred to an optimization issue while the control points to construct the Bézier curve are the design variables. A constrained differential evolution (DE) scheme with premature handling strategy is implemented to find the optimal solution of the design variables while specific objectives and imposed constraints are satisfied. Differ from traditional methods, we synthesize null-space and specialized curve to provide a novel viewpoint for trajectory planning of free-floating space robot. Simulation results are presented for trajectory planning of 7 degree-of-freedom (DOF) kinematically redundant manipulator mounted on a free-floating spacecraft and demonstrate the feasibility and effectiveness of the proposed method. 相似文献
240.