全文获取类型
收费全文 | 1673篇 |
免费 | 288篇 |
国内免费 | 466篇 |
专业分类
航空 | 694篇 |
航天技术 | 653篇 |
综合类 | 121篇 |
航天 | 959篇 |
出版年
2024年 | 10篇 |
2023年 | 54篇 |
2022年 | 58篇 |
2021年 | 100篇 |
2020年 | 69篇 |
2019年 | 109篇 |
2018年 | 120篇 |
2017年 | 102篇 |
2016年 | 101篇 |
2015年 | 122篇 |
2014年 | 214篇 |
2013年 | 137篇 |
2012年 | 166篇 |
2011年 | 137篇 |
2010年 | 125篇 |
2009年 | 118篇 |
2008年 | 100篇 |
2007年 | 80篇 |
2006年 | 66篇 |
2005年 | 95篇 |
2004年 | 34篇 |
2003年 | 50篇 |
2002年 | 39篇 |
2001年 | 32篇 |
2000年 | 29篇 |
1999年 | 22篇 |
1998年 | 19篇 |
1997年 | 13篇 |
1996年 | 11篇 |
1995年 | 11篇 |
1994年 | 13篇 |
1993年 | 7篇 |
1992年 | 6篇 |
1991年 | 10篇 |
1990年 | 12篇 |
1989年 | 10篇 |
1988年 | 7篇 |
1987年 | 1篇 |
1986年 | 1篇 |
1985年 | 17篇 |
排序方式: 共有2427条查询结果,搜索用时 125 毫秒
991.
Reconstructed attitude data for the Hipparcos mission as obtained in the final stages of the data analysis for the published
catalogue is used to derive detailed information on the dynamics of the satellite. Most elements of the inertia tensor of
the satellite could be calibrated from the observed acceleration data, which are also used to reconstruct torques due to solar
radiation and gravity gradient, and the magnetic moment of the satellite and it's interaction with the magnetic field surounding
the Earth. The effects of the oblateness of the Earth on the gravity gradient are evaluated and shown to be negligable. The
magnetic field model includes both the `main' and the `disturbance' fields. The remaining systematic effects in residual torques
are most likely attributed to variations in the magnetic field that are local and are beyond the models used to describe it.
The angular momentum vector for one of the gyros was reconstructed from the torque it asserted on the satellite while it was
running in redundant mode.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
992.
993.
994.
995.
本文采用时间相关法和隐式推进迭代方法求解了绕HERMES外形高超声速无粘流动。将抛物型方程和代数方程相结合生成计算网格,既节省了网格生成的时间,又能得到较合理的网格分布。在时间相关法计算中,采用了显式NND格式;在隐式推进迭代计算中,采用了推广的隐式NND格式。 相似文献
996.
The Geospace Double Star Project (DSP) consists of two small satellites operating in the near-earth equatorial and polar regions, respectively. The goals of DSP are: (1) to provide high-resolution field, particle, and wave measurements in some important near-earth active regions which have not been covered by current ISTP missions, such as the near-earth plasma sheet and its boundary layer, the ring current, the radiation belts, the dayside magnetopause boundary layer, and the polar region; (2) to investigate the trigger mechanisms of magnetic storms, magnetospheric substorms, and magnetospheric particle events,as well as the responses of geospace storms to solar activities and interplanetary disturbances; (3) to set up the models describing the spatial and temporal variations of the near-earth space environment.To realize the above goals, the equatorial satellite TC-1 and the polar satellite TC-2 will accommodate, respectively, eight instruments on board. TC-1was launched successfully in December 2003 while the polar satellite (TC-2)will be launched in July 2004. The orbit of the equatorial satellite TC-1 consists of a perigee at 550 km, an apogee at 60 000 km, and an inclination of about 28.5; while the orbit of the polar satellite will have a perigee of 700 km, an apogee of 40 000 km, and an inclination of about 90. The two satellites will take coordinated measurements with Cluster Ⅱ and will first form a "six-point exploration" in geospace.The operational status of TC-1 are introduced in this paper. 相似文献
997.
航天发射用磁悬浮助推发射系统概念研究 总被引:4,自引:2,他引:4
针对日益增加的航天发射成本问题和安全、可靠、低成本航天发射方式的需求,阐述了磁悬浮助推发射概念及其优越性.初步分析了磁悬浮助推发射系统组成及各分系统功能.通过比较电磁悬浮(EMS)和超导电动(EDS)两种磁悬浮系统性能,结果表明EDS是更适合于磁悬浮助推发射的磁悬浮系统方案.通过助推发射能量需求初步分析,直线电机加速能量供给系统是难题之一,需要重点解决.采用飞行弹道分析方法,说明地面助推水平起飞单级入轨运载器方案的可行性及特点.与其它航天助推发射方式比较,磁悬浮助推发射在提高入轨载荷和降低发射成本方面具有优势. 相似文献
998.
针对深空探测器姿态估计问题,提出了一种基于星敏感器的深空飞行器姿态估计新型算法,用李群替代了传统的四元数来描述姿态,避免了四元数转换为姿态矩阵产生的非唯一性和复杂计算等问题。该算法给出了基于星敏感器的姿态观测方程和空间中刚体的运动学模型在李群下的描述并提出了一种基于李群的滤波算法,完成了深空飞行器动态姿态的确定。该线性化模型解决了传统非线性模型在滤波过程中产生的误差,同时省去了四元数转化为姿态矩阵的步骤,减少了计算量。最后,仿真实验中对比了传统的基于四元数的姿态确定算法,可以看出该算法具有更好的稳定性和准确性。 相似文献
999.
D.B. Contreira F.S. Rodrigues K. Makita C.G.M. Brum W. Gonzalez N.B. Trivedi M.R. da Silva N.J. Schuch 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2005,36(12):2455-2459
The occurrence of radio signal fading events caused by ionospheric absorption plays an important role in the performance of radio-communication systems. It is necessary to know the magnitude and time-scale of such events in order to specify technical parameters of the communication system to be used. Generally, fading events are associated with solar flares, which are characterized by sudden increase in the solar X-ray flux that causes an increase in the ionization in the lower ionosphere. The abrupt increase of ionization causes the absorption of radio waves propagating in the Earth–ionosphere wave-guide and is reported as radio signal fading events. A simple experiment to monitor the behavior of lower ionosphere has been carried out at the Southern Space Observatory-SSO/INPE (29.43°S, 53.8°W), located in southern Brazil. The experiment is basically a computer controlled radio receiver that records the received signal strength of Amplitude Modulated (AM) radio signals in the HF (High Frequencies) range. We analyzed data of the 6 MHz beacon signal that has been transmitted by a broadcasting radio station located about 400 km from the observation site. In this work we present initial results of daily variation of the received signal strength and fading events associated with solar flares observed in the 6 MHz signal monitored by the experiment during 2001. X-ray solar flux data from the GOES-8 satellite were used to identify X-ray solar bursts associated with solar flares. Based on the one-year data collected by the experiment, a statistical summary of fading occurrences and their correlation with solar flares, as well as the distributions of time-scales and magnitudes of such events are presented. 相似文献
1000.
为了获得空间目标的微动信息,需要对雷达回波中的高速平动分量进行精确补偿。针对空间目标高速运动对微动信息提取的影响问题,首先分析了空间目标平动对微多普勒频率的调制影响,得到目标高速平动,特别是平动加速度、平动加加速度对微多普勒频率趋势性调制现象将干扰微多普勒频率提取的结论。在此基础上,利用目标平动直接导致目标多普勒频谱展宽的特点,提出了一种基于图像质量度量准则的空间目标平动参数估计方法,并根据估计出的平动参数实现运动补偿。最后,采用空间目标多散射中心模型,进行平动补偿分析,仿真结果验证了该方法的有效性。 相似文献