全文获取类型
收费全文 | 744篇 |
免费 | 170篇 |
国内免费 | 192篇 |
专业分类
航空 | 525篇 |
航天技术 | 209篇 |
综合类 | 111篇 |
航天 | 261篇 |
出版年
2024年 | 5篇 |
2023年 | 15篇 |
2022年 | 31篇 |
2021年 | 53篇 |
2020年 | 32篇 |
2019年 | 31篇 |
2018年 | 37篇 |
2017年 | 47篇 |
2016年 | 24篇 |
2015年 | 35篇 |
2014年 | 61篇 |
2013年 | 41篇 |
2012年 | 52篇 |
2011年 | 52篇 |
2010年 | 56篇 |
2009年 | 50篇 |
2008年 | 59篇 |
2007年 | 43篇 |
2006年 | 44篇 |
2005年 | 23篇 |
2004年 | 14篇 |
2003年 | 25篇 |
2002年 | 22篇 |
2001年 | 14篇 |
2000年 | 30篇 |
1999年 | 28篇 |
1998年 | 38篇 |
1997年 | 19篇 |
1996年 | 18篇 |
1995年 | 18篇 |
1994年 | 11篇 |
1993年 | 17篇 |
1992年 | 14篇 |
1991年 | 12篇 |
1990年 | 9篇 |
1989年 | 7篇 |
1988年 | 6篇 |
1987年 | 7篇 |
1986年 | 1篇 |
1985年 | 1篇 |
1984年 | 1篇 |
1982年 | 1篇 |
1981年 | 1篇 |
1965年 | 1篇 |
排序方式: 共有1106条查询结果,搜索用时 281 毫秒
652.
When manned spacecraft comes back to the earth, it relies on the impact attenuation seat to protect astronauts from injuries during landing phase. Hence, the seat needs to transfer impact load, as small as possible, to the crew. However, there is little room left for traditional seat to improve further. Herein, a new seat system biologically-inspired by felids’ landing is proposed.Firstly, a series of experiments was carried out on cats and tigers, in which they were trained to jump down voluntarily from different heights. Based on the ground reaction forces combined with kinematics, the experiment indicated that felids’ landing after self-initial jump was a multi-step impact attenuation process and the new seat was inspired by this. Then the construction and work process of new seat were redesigned to realize the multi-step impact attenuation. The dynamic response of traditional and new seat is analyzed under the identical conditions and the results show that the new concept seat can significantly weaken the occupant overload in two directions compared with that of traditional seat. As a consequence, the risk of injury evaluated for spinal and head is also lowered, meaning a higher level of protection which is especially beneficial to the debilitated astronaut. 相似文献
653.
A new simple and effective inertial parameter identification method based on sinusoidal vibrations of a six-degree-of-freedom parallel manipulator is proposed. Compared with previously known identification algorithms, the advantages of the new approach are there is no need to design the excitation trajectory to consider the condition number of the observation matrix and the inertial matrix can be accurately defined regardless of the effect of viscous friction. In addition, the use of a sinusoidal exciting trajectory allows calculation of the velocities and accelerations from the measured position response. Simulations show that the new approach has acceptable tolerance of dry friction when using a simple coupling parameter modified formula. The experimental application to the hydraulically driven Stewart platform demonstrates the capability and efficiency of the proposed identification method. 相似文献
654.
柯志强崔卫军廉伟 《民用飞机设计与研究》2015,(2):20-23
将翼盒尺寸设计中多学科设计要求,包括应力、稳定性、气动弹性、变形和制造等要求转化为优化设计过程中和结构尺寸相关联的约束条件,从而将翼盒尺寸多学科优化设计(MDO)问题转化为多约束优化设计(MCO)问题。基于Hyperworks优化设计平台,建立了某型飞机翼盒有限元模型并利用TCL\TK语言将多学科约束嵌入到翼盒尺寸优化设计过程中,定义了多约束优化设计模型。优化设计结果减重7.4%,有效指导了翼盒结构详细设计。 相似文献
655.
656.
介绍网带炉在静态不充气、充气及动态充气等状态下,温场的测量方法;并就冷态空载、负载运行时间及加热空载、负载运行时间的测量进行了讨论和分析。 相似文献
657.
658.
659.
Ruhai Wang Stephen Horan Bingxin Tian Sreelakshmi Bonasu 《IEEE transactions on aerospace and electronic systems》2006,42(4):1311-1322
The acknowledgement (ACK) strategy of transmission control protocol (TCP) has been modified to delay the ACKs for a configurable period of time that is related to the round-trip time (RTT) to improve its performance in asymmetric links such as space communications. A general relationship between the asymmetric channel ratio and the optimal ACK frequency to achieve maximum throughput is not available. This paper studies the optimal ACK frequency with respect to the channel RTT to achieve the maximum throughput over various asymmetric, geo-stationary earth orbit (GEO)-satellite links using a test-bed. It is found that when the asymmetric channel ratio is as high as about 100/1, the optimal ACK frequency must be increased with an increase in asymmetric ratio to complement the impact of the reduction of ACK channel rate. As a rule of thumb, every two-fold increase in asymmetric ratio requires the optimal ACK frequency to be increased by one ACK per RTT. A regression model was built to reflect the relationship between the optimal ACK frequency and the asymmetric channel ratio and has been validated 相似文献
660.
真空实验舱数字式压力控制系统设计与验证 总被引:1,自引:0,他引:1
针对脉冲等离子体推力器测试所需的容积大于60m3的大型真空实验舱对气压控制的要求,设计了数字式压力控制系统.该控制系统采用旋片泵组和罗茨泵构成两级串联的组合抽气方式对实验舱进行抽真空,具有较高的效率.基于双曲正切函数构建了变增益函数,从而实现对不同压力范围的变增益比例、积分和微分(PID)调节.试验结果表明,这一数字式... 相似文献