全文获取类型
收费全文 | 1629篇 |
免费 | 267篇 |
国内免费 | 236篇 |
专业分类
航空 | 941篇 |
航天技术 | 568篇 |
综合类 | 126篇 |
航天 | 497篇 |
出版年
2024年 | 6篇 |
2023年 | 30篇 |
2022年 | 43篇 |
2021年 | 56篇 |
2020年 | 68篇 |
2019年 | 58篇 |
2018年 | 80篇 |
2017年 | 75篇 |
2016年 | 71篇 |
2015年 | 76篇 |
2014年 | 110篇 |
2013年 | 88篇 |
2012年 | 141篇 |
2011年 | 132篇 |
2010年 | 94篇 |
2009年 | 85篇 |
2008年 | 86篇 |
2007年 | 95篇 |
2006年 | 97篇 |
2005年 | 104篇 |
2004年 | 64篇 |
2003年 | 46篇 |
2002年 | 60篇 |
2001年 | 48篇 |
2000年 | 34篇 |
1999年 | 33篇 |
1998年 | 44篇 |
1997年 | 28篇 |
1996年 | 23篇 |
1995年 | 21篇 |
1994年 | 28篇 |
1993年 | 17篇 |
1992年 | 16篇 |
1991年 | 23篇 |
1990年 | 23篇 |
1989年 | 9篇 |
1988年 | 12篇 |
1987年 | 6篇 |
1986年 | 2篇 |
排序方式: 共有2132条查询结果,搜索用时 0 毫秒
941.
942.
基于均匀加权天线模型,推导星载ScanSAR天线指向不稳定引起的多普勒中心频率估计误差,建立多普勒中心频率估计误差与图像辐射校正精度之间的数学模型,进而提出星载ScanSAR辐射校正对天线指向稳定度的要求。最后,通过计算机仿真,验证了理论分析的正确性。 相似文献
943.
基于连续激光源的高采样频率DPIV系统在进行曝光时可能会产生粒子拖尾现象。明渠湍流试验和数值模拟试验结果显示,粒子拖尾长度的增加会导致平均流速减小和湍流强度增大。分析表明,导致平均流速误差的原因之一是诊断窗口边缘局部粒子图像的缺失,且图像缺失程度会随着粒子拖尾长度增加而增大,从而使平均速度随粒子拖尾长度增加而减小;粒子拖尾的另一个直接后果是增大了粒子图像的有效粒径,从而导致湍流强度增大。通过增大第二个诊断窗口的尺寸,进行相关函数标准化和相关系数补偿等方法,可以消除粒子拖尾长度引起的误差。 相似文献
944.
Estrella Olmedo Noelia Sánchez-Ortiz Nuria Guijarro Jaime Nomen Holger Krag 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
In the framework of a potential European Space Situational Awareness System (ESSAS), we propose some optical strategies such that try to minimize the requirement of tracking measurements for the orbit determination computation when the catalogue is under construction. We will analyse them in terms of coverage, timeliness and orbit determination accuracy by means of the AS4 simulator (developed by Deimos Space S.L.U.). Moreover, observation campaigns have been performed from La Sagra Observatory in order to check the applicability of those strategies. These strategies are used for defining different choices for the future European Optical Space Surveillance System in the framework of the ESA contract no. 22738/09/D/HK. 相似文献
945.
In this paper, a modified unscented Kalman filter (UKF) for nonlinear stochastic systems is proposed, and it is applied to autonomous orbit determination for Earth satellites. Based on some standard results about the boundedness of stochastic processes and a new formulation of the unscented transformation (UT), it is demonstrated that the design of the noise covariance matrix plays an important role in enhancing the filter stability. Furthermore, a particular design of the noise covariance matrix is proposed as a modification of the UKF. The modified UKF is less sensitive to the initial error than the usual one. High performance of the modified UKF is illustrated in comparison with the usual one by using the real data obtained from an Earth sensor. 相似文献
946.
947.
Lu Cao Xiaoqian Chen Arun K. Misra 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
Attitude determination is one of the key technologies for Attitude Determination and Control System (ADCS) of a satellite. However, serious model errors may exist which will affect the estimation accuracy of ACDS, especially for a small satellite with low precision sensors. In this paper, a central difference predictive filter (CDPF) is proposed for attitude determination of small satellites with model errors and low precision sensors. The new filter is proposed by introducing the Stirling’s polynomial interpolation formula to extend the traditional predictive filter (PF). It is shown that the proposed filter has higher accuracy for the estimation of system states than the traditional PF. It is known that the unscented Kalman filter (UKF) has also been used in the ADCS of small satellites with low precision sensors. In order to evaluate the performance of the proposed filter, the UKF is also employed to compare it with the CDPF. Numerical simulations show that the proposed CDPF is more effective and robust in dealing with model errors and low precision sensors compared with the UKF or traditional PF. 相似文献
948.
传统的译文质量自动评测方法主要针对机器自动翻译结果并通过与参考译文的对比实现译文质量的评估。提出一种大规模无参考译文质量自动评测方法,该方法可以在无参考译文的情况下,从正确性、流畅性和忠实度等方面对人工译文进行质量检查并标注可能的错误点,即利用语言规则实现正确性的判断,利用语言模型实现流畅性的判断,利用词对齐结果和词典信息实现忠实度的判断。基于该方法实现的译文质量辅助检查系统在国家知识产权局百万专利翻译项目中的应用效果表明,使用该系统的测试组较未使用该系统的测试组的平均译文质量和终稿完成效率均有明显提升。 相似文献
949.
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
950.
在标定捷联惯组加速度计时,一般采用多位置试验,但是目前并未对多位置试验所能标定出的误差系数数量和标定结果的有效性进行分析,本文针对这一问题展开了研究.首先,阐述了带有高次误差项的捷联惯组加速度计误差模型.然后,针对一般6位置标定方法无法完成这一模型标定的缺陷,提出了一种18位置标定方法.进行标定后,运用显著性分析方法,对误差模型本身和其中的参数的有效性进行了分析.最后,通过重复进行去除最不显著项、再标定、显著性检验等步骤,获得了试验室条件下所能标定的捷联惯组加速度计组合误差模型. 相似文献