全文获取类型
收费全文 | 120篇 |
免费 | 97篇 |
国内免费 | 40篇 |
专业分类
航空 | 186篇 |
航天技术 | 19篇 |
综合类 | 10篇 |
航天 | 42篇 |
出版年
2023年 | 2篇 |
2022年 | 13篇 |
2021年 | 26篇 |
2020年 | 15篇 |
2019年 | 13篇 |
2018年 | 10篇 |
2017年 | 5篇 |
2016年 | 11篇 |
2015年 | 5篇 |
2014年 | 9篇 |
2013年 | 9篇 |
2012年 | 14篇 |
2011年 | 11篇 |
2010年 | 11篇 |
2009年 | 8篇 |
2008年 | 9篇 |
2007年 | 6篇 |
2006年 | 8篇 |
2005年 | 8篇 |
2004年 | 3篇 |
2003年 | 7篇 |
2002年 | 12篇 |
2001年 | 7篇 |
2000年 | 6篇 |
1999年 | 6篇 |
1998年 | 9篇 |
1997年 | 6篇 |
1996年 | 1篇 |
1993年 | 2篇 |
1992年 | 1篇 |
1991年 | 4篇 |
排序方式: 共有257条查询结果,搜索用时 31 毫秒
101.
转速是液体火箭发动机试车的重要特征参数,通过讨论发动机即时转速的时域计数法、频谱最大法、相位残差等三种方法的优缺点以及误差分析,提出了将三种方法有机结合起来的综合算法,并将该方法应用到两种液体火箭发动机涡轮泵转速的处理中。实践证明,综合处理方法继承了各种方法的优点,避免了它们的缺点,具有工程实用价值。 相似文献
102.
Benjamin Lenoir Bruno Christophe Serge Reynaud 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
The Gravity Advanced Package is an instrument composed of an electrostatic accelerometer called MicroSTAR and a rotating platform called Bias Rejection System. It aims at measuring with no bias the non-gravitational acceleration of a spacecraft. It is envisioned to be embarked on an interplanetary spacecraft as a tool to test the laws of gravitation. 相似文献
103.
Casing treatment is a mature stabilization technique which has been widely applied on aero-engines for modern aircrafts and turbo-chargers for automobiles. After the investigations of half century since the 1960s, this technique has been well developed for various configurations with different effectiveness. From the perspective of stabilization mechanism, this paper roughly categorizes the configurations of casing treatment into two types: traditional ones which work by affecting the flow structure of blade tip region; a novel one named as Stall Precursor-Suppressed (SPS) casing treatment. The effectiveness of both types will be demonstrated for their applications on axial compressors and centrifugal compressors with uniform or distorted inlet. And the stabilization mechanism of casing treatments for regular types and SPS one will also be explained respectively. In addition, this review will summarize the methodologies of casing treatments with the numerical simulations for regular grooved configurations and the eigenvalue approach for SPS casing treatment. Looking forward to the future of compressor stabilization, casing treatment technique will still exist as a general and inexpensive option, and the exploration for its effectiveness and mechanism will be deeper with the development of computational fluid dynamics and advanced measurement techniques. 相似文献
104.
阐述了控制惯导系统中多余物的重要性,分析了在操作过程中惯导系统多余物产生的条件和因素,根据多年的惯导系统生产经验,总结了控制多余物的实际操作要求,最后叙述了对多余物常用检查方法及使用MORET-300活动多余物检测设备的方法。 相似文献
105.
106.
107.
空间对接试验台转动模拟装置的试验研究 总被引:2,自引:0,他引:2
针对空间对接试验台中二维转动实现的设计难点问题,提出了非常规应用的新型抗弯件及十字轴机械结构方案。使整个系统在大负载和高撞击力的特殊情况下,结构具有高可靠性;大大降低了转动摩擦力矩,使转动模拟装置具有良好的随动运动特性;结构尺寸紧凑,减小了与结构尺寸关系密切的航天器惯量模拟误差;质量轻,使试验台其余子系统的设计有一定余量。采用缩比方法研制了试验装置。试验结果表明,主动转动模拟装置的最大静摩擦力矩仅为8.8445Nm,远小于80 Nm的指标要求。所设计的转动模拟装置能够满足对接试验台总体和其它分系统的要求。 相似文献
108.
本文介绍了八工位聚氨酯注塑回转自动生产线中回转盘系统的总体设计思路及各部件的结构设计,该系统具有运行平稳,定位准确和制造简单的特点。 相似文献
109.
110.
Zhouzheng Gao Tuan Li Hongping Zhang Maorong Ge Harald Schuh 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(9):2393-2405
Since China’s BeiDou satellite navigation system (BDS) began to provide regional navigation service for Asia-Pacific region after 2012, more new generation BDS satellites have been launched to further expand BDS’s coverage to be global. In this contribution, precise positioning models based on BDS and the corresponding mathematical algorithms are presented in detail. Then, an evaluation on BDS’s real-time dynamic positioning and navigation performance is presented in Precise Point Positioning (PPP), Real-time Kinematic (RTK), Inertial Navigation System (INS) tightly aided PPP and RTK modes by processing a set of land-borne vehicle experiment data. Results indicate that BDS positioning Root Mean Square (RMS) in north, east, and vertical components are 2.0, 2.7, and 7.6?cm in RTK mode and 7.8, 14.7, and 24.8?cm in PPP mode, which are close to GPS positioning accuracy. Meanwhile, with the help of INS, about 38.8%, 67.5%, and 66.5% improvements can be obtained by using PPP/INS tight-integration mode. Such enhancements in RTK/INS tight-integration mode are 14.1%, 34.0%, and 41.9%. Moreover, the accuracy of velocimetry and attitude determination can be improved to be better than 1?cm/s and 0.1°, respectively. Besides, the continuity and reliability of BDS in both PPP and RTK modes can also be ameliorated significantly by INS during satellite signal missing periods. 相似文献