全文获取类型
收费全文 | 469篇 |
免费 | 105篇 |
国内免费 | 46篇 |
专业分类
航空 | 249篇 |
航天技术 | 205篇 |
综合类 | 20篇 |
航天 | 146篇 |
出版年
2024年 | 2篇 |
2023年 | 12篇 |
2022年 | 20篇 |
2021年 | 30篇 |
2020年 | 36篇 |
2019年 | 19篇 |
2018年 | 10篇 |
2017年 | 23篇 |
2016年 | 27篇 |
2015年 | 26篇 |
2014年 | 31篇 |
2013年 | 29篇 |
2012年 | 37篇 |
2011年 | 32篇 |
2010年 | 33篇 |
2009年 | 32篇 |
2008年 | 27篇 |
2007年 | 20篇 |
2006年 | 28篇 |
2005年 | 22篇 |
2004年 | 22篇 |
2003年 | 20篇 |
2002年 | 7篇 |
2001年 | 8篇 |
2000年 | 6篇 |
1999年 | 12篇 |
1998年 | 9篇 |
1997年 | 4篇 |
1996年 | 4篇 |
1995年 | 8篇 |
1994年 | 12篇 |
1993年 | 2篇 |
1992年 | 2篇 |
1991年 | 3篇 |
1989年 | 2篇 |
1988年 | 1篇 |
1984年 | 2篇 |
排序方式: 共有620条查询结果,搜索用时 593 毫秒
231.
232.
《中国航空学报》2021,34(4):306-319
A nonlinear dynamic modeling method for primary mirror of Flower-like Deployable Space Telescope (F-DST) undergoing large deployment motion is proposed in this paper. To ensure pointing accuracy and attitude stability of the paraboloidal primary mirror, the mirror is discretized into equal thickness shell elements by considering shell curvature. And the material nonlinear constitutive relation of flexible mirror is acquired using Absolute Nodal Coordinate Formulation (ANCF). Furthermore, the primary mirror of F-DST can be regarded as a clustered multi-body system, and its dynamic equations of elastic deformation and deployment motion are established by virtual work principle. Finally, the deployment motion of primary mirror by different driving conditions are simulated, the results show that the vibrations of mirrors that driven by elastic hinge device are more than that driven by servo motor. In addition, single sub-mirror deployment process will perturb the pointing accuracy of primary mirror, and the multiple sub-mirrors simultaneously deploying will seriously affect all the sub-mirrors surface accuracy because of the coupling effect. Thus, there are theoretical value and practical significance for the controlling surface accuracy and attitude accuracy of space telescope. 相似文献
233.
234.
The carrier synchronization algorithm of the autonomous radio for deep space is studied. When the signal modulation is unknown, this paper improves the existing universal carrier synchronization loop for multiple modulations, expands the frequency tracking range of the loop, proposes a Tong detection-based M-ary Phase Shift Keying (M-PSK) signal locking detection algorithm to rapidly and effectively determine whether the current phase discrimination mode matches the modulation mode, so as to independently choose whether to switch the phase discrimination mode. Through theoretical analysis and comparison, it is described that the total detection probability of the algorithm proposed in this paper is significantly higher than the probability of single lock detection. Simulation results show that the algorithm has high detection probability and low computational complexity at a low signal to noise ratio. 相似文献
235.
Two groups of microwave type U and Reverse-Slope (RS) bursts after the Soft X-Ray (SXR) maximum were observed with the 2.6~3.8GHz spectrometer of Chinese Solar Broadband Radio Spectrometers (SBRS/Huairou) on 15 February 2011, when an X2.2 solar flare occurred in the Active Region (AR) NOAA11158. A Shear-driven Quadrupolar Reconnection (SQR) model was utilized to analyze these bursts and the two loops involved were found to be basically in the same spatial scale and have a height difference of about 1300km. These bursts were interpreted to be a result of a new reconnection process between the two similar-scaled loops. 相似文献
236.
以星载大型索网式可展开天线为对象,研究在轨工作过程中天线视轴高精度高稳定度指向控制方法。首先,基于Craig-Bampton法建立表征天线指向的动力学模型;然后针对天线振动对视轴指向的影响,设计PD反馈+陷波滤波器的控制算法;进一步分析影响指向精度的因素,设计带有调节滤波器的改进控制器以减小天线视轴指向的周期性误差,提高指向精度与稳定度。最后,给出数值仿真校验的结果并与现有的方法进行比较。结果表明,所提出的控制算法在保证天线指向稳定的同时,可以有效减小天线视轴的指向偏差,并对干扰与振动具有良好的鲁棒性。 相似文献
237.
针对存在系统参数不确定与外界干扰的航天器大角度姿态机动问题,提出一种基于干扰估计的鲁棒次优控制方法。该方法通过引入总干扰的概念,将不确定参数与外界干扰对系统的影响统一为各控制通道总干扰,而后采用非线性干扰观测器实现对系统总干扰的估计;借鉴状态相关的黎卡提方程(SDRE)方法,将系统模型改写为状态相关的线性形式,并采用近似方法实现基于干扰估计的次优控制参数的在线求解。通过对航天器大角度姿态机动问题的仿真分析,校验所提方法不仅较传统SDRE方法计算效率更高,而且较大程度上提高系统对参数偏差与外界干扰的鲁棒性能。 相似文献
238.
239.
240.