全文获取类型
收费全文 | 1382篇 |
免费 | 156篇 |
国内免费 | 150篇 |
专业分类
航空 | 501篇 |
航天技术 | 577篇 |
综合类 | 43篇 |
航天 | 567篇 |
出版年
2023年 | 36篇 |
2022年 | 32篇 |
2021年 | 65篇 |
2020年 | 51篇 |
2019年 | 40篇 |
2018年 | 47篇 |
2017年 | 40篇 |
2016年 | 53篇 |
2015年 | 58篇 |
2014年 | 68篇 |
2013年 | 72篇 |
2012年 | 80篇 |
2011年 | 94篇 |
2010年 | 79篇 |
2009年 | 66篇 |
2008年 | 70篇 |
2007年 | 94篇 |
2006年 | 69篇 |
2005年 | 93篇 |
2004年 | 56篇 |
2003年 | 57篇 |
2002年 | 45篇 |
2001年 | 37篇 |
2000年 | 54篇 |
1999年 | 34篇 |
1998年 | 31篇 |
1997年 | 27篇 |
1996年 | 26篇 |
1995年 | 22篇 |
1994年 | 19篇 |
1993年 | 15篇 |
1992年 | 10篇 |
1991年 | 18篇 |
1990年 | 5篇 |
1989年 | 6篇 |
1988年 | 7篇 |
1987年 | 6篇 |
1986年 | 1篇 |
1984年 | 5篇 |
排序方式: 共有1688条查询结果,搜索用时 18 毫秒
81.
A new global approach for rendezvous Linear Quadratic controller design is presented in this paper. Instead of solving the algebraic Riccati equation, a continuous simulated annealing (SA) algorithm is used to design rendezvous LQ controller. Optimization of one automatic rendezvous controller with 18 design parameters is illustrated. The results show that the SA algorithm can locate the global solution effectively and robust, besides a great number of global solutions have been obtained by the SA. The SA has demonstrated better performance than other optimization algorithms such as floating-coded Genetic Algorithm, Simplex method and Powell algorithm. 相似文献
82.
83.
84.
Sean C. Solomon Ralph L. McNutt Jr. Robert E. Gold Deborah L. Domingue 《Space Science Reviews》2007,131(1-4):3-39
The MErcury Surface, Space ENvironment, GEochemistry, and Ranging (MESSENGER) spacecraft, launched on August 3, 2004, is nearing the halfway point on its voyage to become the first probe to orbit the planet Mercury. The mission, spacecraft, and payload are designed to answer six fundamental questions regarding the innermost planet: (1) What planetary formational processes led to Mercury’s high ratio of metal to silicate? (2) What is the geological history of Mercury? (3) What are the nature and origin of Mercury’s magnetic field? (4) What are the structure and state of Mercury’s core? (5) What are the radar-reflective materials at Mercury’s poles? (6) What are the important volatile species and their sources and sinks near Mercury? The mission has focused to date on commissioning the spacecraft and science payload as well as planning for flyby and orbital operations. The second Venus flyby (June 2007) will complete final rehearsals for the Mercury flyby operations in January and October 2008 and September 2009. Those flybys will provide opportunities to image the hemisphere of the planet not seen by Mariner 10, obtain high-resolution spectral observations with which to map surface mineralogy and assay the exosphere, and carry out an exploration of the magnetic field and energetic particle distribution in the near-Mercury environment. The orbital phase, beginning on March 18, 2011, is a one-year-long, near-polar-orbital observational campaign that will address all mission goals. The orbital phase will complete global imaging, yield detailed surface compositional and topographic data over the northern hemisphere, determine the geometry of Mercury’s internal magnetic field and magnetosphere, ascertain the radius and physical state of Mercury’s outer core, assess the nature of Mercury’s polar deposits, and inventory exospheric neutrals and magnetospheric charged particle species over a range of dynamic conditions. Answering the questions that have guided the MESSENGER mission will expand our understanding of the formation and evolution of the terrestrial planets as a family. 相似文献
85.
86.
本文建立某型飞机Ⅱ梁框结构裂纹形成寿命NP 与裂纹扩展寿命N P 之间的可靠度模型 ,将安全寿命设计与损伤容限设计原理有机结合 ,计算了在给定结构可靠度下该型飞机机翼Ⅱ梁框的检修周期 相似文献
87.
介绍了在水洞中进行的二维机翼纯俯仰运动和沉浮/俯仰联合运动时的流动显示实验.实验结果揭示了机翼做纯俯仰运动时尾迹涡街的特性以及与Strouhal数(Ste)的关系.在Ste=0.105附近,涡街排列成一条线;大于该值,为逆Karman涡街;小于该值,为正Karman涡街.机翼做沉浮/俯仰联合运动时,尾迹中总是出现逆Karman涡街.结合数值计算结果说明,机翼做沉浮/俯仰联合运动时,推力及最大有效迎角与沉浮和俯仰运动之间的相位差有关.并讨论了前缘涡与后缘涡相互作用对推力的影响. 相似文献
88.
航天器在地面待发射期间和空间实际飞行过程中,热控元件光学太阳反射器要遇到各种地面和空间环境,为了航天器的可靠和长寿命,必须对所制备的OSR涂层进行各种地面和空间环境试验并对其各项性能检验与考核,该文就这一系列试验的目的和规范进行了讨论。 相似文献
89.
Nathan R. Boone Robert A. Bettinger 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(8):2319-2332
The theoretical analysis of the motion of natural space debris near the stable Earth-Moon Lagrange Points, and , is presented with a focus on the potential debris risks to spacecraft operating near these points. Specifically, the research formulates a debris propagation model using four-body dynamics, then applies candidate probabilistic survivability models to a notional spacecraft operating at the and Lagrange points to quantify the collision risks to the spacecraft from natural debris particles. Of the survivability models implemented, the natural debris collision risks to spacecraft survivability are found to be incredibly low, but mitigation strategies to reduce the risk further are identified in this study. Overall, research into stable Lagrange point natural debris propagation improves understanding of the collision risks posed by the naturally occurring Kordylewski clouds and enhances operational planning for Lagrange point space missions. 相似文献
90.