全文获取类型
收费全文 | 1088篇 |
免费 | 296篇 |
国内免费 | 202篇 |
专业分类
航空 | 928篇 |
航天技术 | 224篇 |
综合类 | 124篇 |
航天 | 310篇 |
出版年
2024年 | 8篇 |
2023年 | 21篇 |
2022年 | 45篇 |
2021年 | 41篇 |
2020年 | 51篇 |
2019年 | 55篇 |
2018年 | 32篇 |
2017年 | 42篇 |
2016年 | 52篇 |
2015年 | 53篇 |
2014年 | 77篇 |
2013年 | 62篇 |
2012年 | 75篇 |
2011年 | 91篇 |
2010年 | 63篇 |
2009年 | 74篇 |
2008年 | 79篇 |
2007年 | 78篇 |
2006年 | 63篇 |
2005年 | 44篇 |
2004年 | 39篇 |
2003年 | 34篇 |
2002年 | 46篇 |
2001年 | 40篇 |
2000年 | 25篇 |
1999年 | 37篇 |
1998年 | 42篇 |
1997年 | 27篇 |
1996年 | 29篇 |
1995年 | 28篇 |
1994年 | 23篇 |
1993年 | 26篇 |
1992年 | 24篇 |
1991年 | 27篇 |
1990年 | 10篇 |
1989年 | 12篇 |
1988年 | 7篇 |
1987年 | 3篇 |
1986年 | 1篇 |
排序方式: 共有1586条查询结果,搜索用时 218 毫秒
691.
692.
693.
694.
为有效提高嵌入式静态随机访问存储器(Static Random Access Memory, SRAM)的可靠性,进而确保整个航天电子系统的可靠运行,通过对嵌入式SRAM故障分布特点的分析,给出了一种改进的存储器架构。采用列块修复与行单元修复相配合的方法,并在此基础上提出了二维冗余模块存在故障的内建冗余分析( Built\|In Redundancy Analysis, BIRA)策略。该策略高效运用了设置的行修复寄存器与列修复寄存器,极大地提高了故障的修复率。通过64×8位的SRAM仿真实验验证了提出的内建冗余分析策略的可行性,有效确保了系统在冗余模块和主存储器都存在故障的情况下的高可靠运行。
相似文献
相似文献
695.
I. Kim H. Hirayama T. Hanada 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
Japan Aerospace Exploration Agency (JAXA) has proposed an active debris removal using electro-dynamic tether to reduce large space debris in the low-Earth orbit. However, a tether strand is thin but long enough to have a large area so that it is vulnerable to small particles. This vulnerability might be the weakest point of a tether system against orbital debris. In order to overcome this weakest point, a double tether system, in which two tether strands are tied together at even intervals to form equally spaced loops, has been suggested as one of the promising candidates. This paper provides a mathematical approach to estimate the survival probability of a double tether system and then apply the approach to evaluate the mission success rate of the active debris removal using electro-dynamic tether that JAXA has proposed. It can be concluded the countermeasure to get enough success rate can be obtained. The result is simulated for Advanced Earth Observing Satellite II (ADEOS-II) re-entry from 800 km sun synchronized orbit to atmosphere. The simulation shows that mission success rate over 90% can be obtained with number of loops over 1000 and 10 mm clearance between two strands. 相似文献
696.
Zhong Lingwei Liu Yu Li Juan Gu Zuo Jiang Haocheng Wang Haixing Tang Haibin 《中国航空学报》2010,23(1):15-21
Charge exchange(CEX) ions could inflict severe damages on the ion thruster optical system. This article is aimed at investigating the characteristics of the CEX ions and their influences upon the optical system by means of particle-in- cell(PIC) ion simulation and Monte Carlo collision(MCC) methods. The results from numerical simulation indicate that despite the fact that CEX ions appear in the entire beamlet region near the ion optical system, the ones that present themselves downstream of the accelerator grid have good reason for attracting more attention. As their trajectories are significantly affected by the local electric field, a great number of CEX ions are accelerated toward grids resulting in sputtering erosion. When the influences of the CEX ions are considered in the numerical simulation, there could hardly be observed augments in the screen grid current, but the accelerator grid current increases from zero to 1. 4% of the beamlet current. It can be understood from the numerical simulation that the CEX ions formed in the region far downstream of the accelerator grid should be blamed for the erosion on the downstream surface of the accelerator grid. 相似文献
697.
简要分析了氦气流量校准装置的工作原理和结构,对系统的软、硬件及校准流程进行了讨论,提出并详细阐述了其计量容积的标定技术和计算方法,并在主标准器的结构设计上提出了新的思路,使装置的流量测量扩展不确定度可达0.03%(k=2)。 相似文献
698.
Based on magnetometer measurements only, three-axis attitude, rate, and orbit estimation are successfully achieved. A single Augmented Dynamics Extended Kalman Filter (ADEKF) is configured by combining the spacecraft nonlinear attitude dynamics and quaternion kinematics with orbital mechanics. The filter design is adopted for three-axis stabilized spacecraft in low Earth orbits where the aerodynamic drag is the dominant source of disturbances in addition to the spacecraft magnetic residuals. To reduce the computational burden, another Interlaced Extended Kalman Filter (IEKF) is developed to uncouple the attitude/rate from the orbit dynamics. Both filters are implemented using the magnetometer measurements and their corresponding time derivatives. As a part of EgyptSat-1 flight scenario, detumbling and standby modes are used for performance testing of the ADEKF. The concept of local observability is applied to the basic filter and the stability is investigated by incorporating extensive Monte Carlo simulations with uniformly distributed initial conditions. The filter shows the capability of estimating the attitude better than 5 deg and rate of order 0.03 deg/s in each axis. In orbit estimation, the filter is capable of estimating the position with accuracy less than 8 km and velocity upto 5 m/s in each axis. 相似文献
699.
“嫦娥二号”卫星CCD立体相机的关键技术 总被引:1,自引:0,他引:1
文章介绍了中国两次绕月探测中 CCD 立体相机所采用的技术与创新,并与国际同类相机所获取的图像进行了比较;在此基础上详细介绍了“嫦娥二号”(CE-2)卫星CCD立体相机的综合创新集成技术--“单镜头两视角同轨立体成像、时间延迟积分图像传感器(TDICCD)推扫、速高比补偿”,并从工程目标与科学目标出发进行探测灵敏度及成像动态范围的需求分析;根据需求分析确定了总体技术方案,包括光、机、电的优化设计以及对月探测中首次采用TDICCD的技术困难与对策;特别讨论了速高比补偿的方案及实施途径,并进行了在轨试验验证。文章最后分别给出了虹湾地区成像分辨率为1.3m以及全月面分辨率为7m 的代表性图像,图像清晰、层次丰富,显示出中国在对月立体成像技术上取得了显著进步。 相似文献
700.
翁东玲 《郑州航空工业管理学院学报(管理科学版)》2008,26(1):89-95
我国现阶段正依照循序渐进、统筹规划、先易后难、留有余地的原则,分阶段、有选择地逐步推出资本项目开放措施。理论研究和各国实践都证明资本账户的开放是利弊共存的,关键在于如何有效疏导和防范开放带来的系列风险,采取有力措施将资本账户开放的风险降到最低点,保证宏观经济的稳定发展。通过探讨2005年7月21日进行汇率制度改革以来,我国开放资本账户过程中所面临的银行体系风险、资本流动性过剩风险和资本流动逆转风险,提出了防范风险的对策建议。 相似文献