全文获取类型
收费全文 | 7042篇 |
免费 | 309篇 |
国内免费 | 259篇 |
专业分类
航空 | 3930篇 |
航天技术 | 2266篇 |
综合类 | 229篇 |
航天 | 1185篇 |
出版年
2021年 | 89篇 |
2020年 | 57篇 |
2019年 | 80篇 |
2018年 | 158篇 |
2017年 | 103篇 |
2016年 | 76篇 |
2015年 | 87篇 |
2014年 | 157篇 |
2013年 | 219篇 |
2012年 | 234篇 |
2011年 | 271篇 |
2010年 | 226篇 |
2009年 | 302篇 |
2008年 | 345篇 |
2007年 | 231篇 |
2006年 | 230篇 |
2005年 | 234篇 |
2004年 | 181篇 |
2003年 | 230篇 |
2002年 | 187篇 |
2001年 | 240篇 |
2000年 | 162篇 |
1999年 | 199篇 |
1998年 | 201篇 |
1997年 | 165篇 |
1996年 | 189篇 |
1995年 | 232篇 |
1994年 | 203篇 |
1993年 | 142篇 |
1992年 | 158篇 |
1991年 | 92篇 |
1990年 | 75篇 |
1989年 | 145篇 |
1988年 | 69篇 |
1987年 | 67篇 |
1986年 | 64篇 |
1985年 | 197篇 |
1984年 | 150篇 |
1983年 | 129篇 |
1982年 | 133篇 |
1981年 | 176篇 |
1980年 | 58篇 |
1979年 | 41篇 |
1978年 | 50篇 |
1977年 | 53篇 |
1975年 | 58篇 |
1973年 | 42篇 |
1972年 | 51篇 |
1971年 | 42篇 |
1970年 | 44篇 |
排序方式: 共有7610条查询结果,搜索用时 15 毫秒
91.
介绍一种简单有效的纠错编码方法 ,用于资源卫星高密度数字磁记录器 ,使误码率由 10 -6降低到 10 -11,同时介绍它的基本工作原理、实现方案及试验结果。 相似文献
92.
93.
测定钡含量的快速方法 总被引:3,自引:0,他引:3
本文研究了测定钡盐中钡含量的快速方法。该法是基于被测的钡离子与过量的铬酸钠标准溶液反应形成铬酸钡沉淀,剩余的铬酸根离子以溴甲酚绿-甲基红为混合指示剂,用盐酸标准溶液滴定,而间接测定钡的量。该法操作简便、快速,可应用于多种钡盐中钡的测定。 相似文献
94.
Luh J. Y. S. Shafran Joel S. Harvey C. Arthur 《IEEE transactions on aerospace and electronic systems》1968,(2):218-233
This paper considers the problem arising from the design of an autopilot for a large booster. The motion-controlling actuators of the booster have both position and rate limits. The problem is formulated as a bounded phase-coordinate problem and analyzed by the ``backing out of the target' procedure. A method of constructing the optimal control is presented. An example of an oscillatory system with two control inputs is given, and the optimal control is expressed as an explicit time function. 相似文献
95.
The analysis and comments presented in this paper are meant to establish the general communication parameters associated with Martian flyby probes and with lander and manned vehicles. Fundamental data transfer problems are reviewed to define comparisons and trends of tradeoffs for future studies. Selected focal points are based upon the long propagation path length, with inherent time delays, and the high noise produced by the sun. These problems are magnified because large quantities of data must be obtained to satisfy the needs of the scientific community and the curiosity of an interested public. A comparison of two communication systems is provided: the microwave spectrum and the optical spectrum, as represented by the microwaves at 2.3 GHz and the laser at 6328 ?. A method of cost effectiveness or value received from space missions (a criterion of power input for data quantity received) is also presented. 相似文献
96.
从汉译英的赘冗和疏漏问题看汉英语法特征之差异——汉语语法的柔性之于英语语法的刚性 总被引:1,自引:0,他引:1
本文从汉译英的翻译实践出发,从英语译文的错误以及汉英译文对比中,去发现并分析汉语和英语语法特征的差异。论述了英语语法的刚性、显性和汉语语法的柔性、隐性,并从语言对思维的影响的角度,探讨了汉语语言文化的深邃独特和英语语言的缜密精确。 相似文献
97.
The Active Rack Isolation System [ARIS] International Space Station [ISS] Characterization Experiment, or ARIS-ICE for short, is a long duration microgravity characterization experiment aboard the ISS. The objective of the experiment is to fully characterize active microgravity performance of the first ARIS rack deployed on the ISS. Efficient ground and on-orbit command and data handling [C&DH] segments are the crux in achieving the challenging objectives of the mission. The objective of the paper is to provide an overview of the C&DH architectures developed for ARIS-ICE, with the view that these architectures may serve as a model for future ISS microgravity payloads. Both ground and on-orbit segments, and their interaction with corresponding ISS C&DH systems are presented. The heart of the on-orbit segment is the ARIS-ICE Payload On-orbit Processor, ARIS-ICE POP for short. The POP manages communication with the ISS C&DH system and other ISS subsystems and payloads, enables automation of test/data collection sequences, and provides a wide range of utilities such as efficient file downlinks/uplinks, data post-processing, data compression and data storage. The hardware and software architecture of the POP is presented and it is shown that the built-in functionality helps to dramatically streamline the efficiency of on-orbit operations. The ground segment has at its heart special ARIS-ICE Ground Support Equipment [GSE] software developed for the experiment. The software enables efficient command and file uplinks, and reconstruction and display of science telemetry packets. The GSE software architecture is discussed along with its interactions with ISS ground C&DH elements. A test sequence example is used to demonstrate the interplay between the ground and on-orbit segments. 相似文献
98.
The International Space Station (ISS), as the largest international science and engineering program in history, features unprecedented technical, cost, scheduling, managerial, and international complexity. A number of major milestones have been accomplished to date, including the construction of major elements of flight hardware, the development of operations and sustaining engineering centers, astronaut training, and eight Space Shuttle/Mir docking missions. International partner contributions and levels of participation have been baselined, and negotiations and discussions are nearing completion regarding bartering arrangements for services and new hardware. As ISS is successfully executed, it can pave the way for more inspiring cooperative achievements in the future. 相似文献
99.
The high inclination orbit for the International Space Station poses a risk to astronauts on EVA during occasional periods of enhanced high energy particle flux from the sun known as Solar Particle Events. We are currently unable to predict these events within the few-hour lead time required for evasive action. Compounding the threat is the fact that station construction occurs during increasing solar activity and through the peak of the solar cycle. In this paper we present an overview of the risk, the current methods to provide forecasts of SPEs, and potential risk mitigation options. 相似文献
100.
A relatively general formulation for studying the dynamics and control of an arbitrary spacecraft with interconnected flexible bodies has been developed accounting for transient system properties, shift in the center of mass, shear deformations, rotary inertias and geometric nonlinearities. This self-contained, comprehensive, numerical algorithm using system modes is applicable to a large class of spacecraft configurations of contemporary and future interests. Here, versatility of the approach is demonstrated through the dynamics and control studies aimed at the evolving Space Station Freedom. 相似文献