全文获取类型
收费全文 | 704篇 |
免费 | 165篇 |
国内免费 | 102篇 |
专业分类
航空 | 387篇 |
航天技术 | 172篇 |
综合类 | 24篇 |
航天 | 388篇 |
出版年
2024年 | 6篇 |
2023年 | 26篇 |
2022年 | 61篇 |
2021年 | 36篇 |
2020年 | 47篇 |
2019年 | 35篇 |
2018年 | 29篇 |
2017年 | 17篇 |
2016年 | 23篇 |
2015年 | 21篇 |
2014年 | 33篇 |
2013年 | 39篇 |
2012年 | 40篇 |
2011年 | 45篇 |
2010年 | 28篇 |
2009年 | 31篇 |
2008年 | 41篇 |
2007年 | 61篇 |
2006年 | 36篇 |
2005年 | 51篇 |
2004年 | 30篇 |
2003年 | 28篇 |
2002年 | 25篇 |
2001年 | 17篇 |
2000年 | 17篇 |
1999年 | 31篇 |
1998年 | 26篇 |
1997年 | 26篇 |
1996年 | 15篇 |
1995年 | 12篇 |
1994年 | 6篇 |
1993年 | 7篇 |
1992年 | 5篇 |
1991年 | 11篇 |
1990年 | 3篇 |
1989年 | 2篇 |
1988年 | 3篇 |
1987年 | 1篇 |
排序方式: 共有971条查询结果,搜索用时 15 毫秒
171.
This paper presents an adaptive path planner for unmanned aerial vehicles (UAVs) to adapt a real-time path search procedure to variations and fluctuations of UAVs’ relevant performances, with respect to sensory capability, maneuverability, and flight velocity limit. On the basis of a novel adaptability-involved problem statement, bi-level programming (BLP) and variable planning step techniques are introduced to model the necessary path planning components and then an adaptive path planner is developed for the purpose of adaptation and optimization. Additionally, both probabilistic-risk-based obstacle avoidance and performance limits are described as path search constraints to guarantee path safety and navigability. A discrete-search-based path planning solution, embedded with four optimization strategies, is especially designed for the planner to efficiently generate optimal flight paths in complex operational spaces, within which different surface-to-air missiles (SAMs) are deployed. Simulation results in challenging and stochastic scenarios firstly demonstrate the effectiveness and efficiency of the proposed planner, and then verify its great adaptability and relative stability when planning optimal paths for a UAV with changing or fluctuating performances. 相似文献
172.
针对存在未知惯量矩阵和外干扰的刚体航天器姿态跟踪,提出了一种鲁棒自适应控制方法。综合自适应反步法和非线性L2增益干扰抑制方法,用自适应反步法构造系统的Lyapunov函数,获得了具L2增益的鲁棒自适应控制器,以保证姿态跟踪误差系统为一致最终有界稳定,确保估计的航天器惯量参数的有界性,并使从外干扰输入到评价输出的L2增益不大于给定值。仿真结果验证了方法的有效性和可行性。 相似文献
173.
174.
175.
176.
J.C. Pérez A. Cerdeña A. González M. Armas 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
In this work a methodology for inferring water cloud macro and microphysical properties from nighttime MODIS imagery is developed. This method is based on the inversion of a theoretical radiative transfer model that simulates the radiances detected in each of the sensor infrared bands. To accomplish this inversion, an operational technique based on Artificial Neural Networks (ANNs) is proposed, whose main characteristic is the ability to retrieve cloud properties much faster than conventional methods. Furthermore, a detailed study of input data is performed to avoid different sources of errors that appear in several MODIS infrared channels. Finally, results of applying the proposed method are compared with in-situ measurements carried out during the DYCOMS-II field experiment. 相似文献
177.
自适应模型跟踪控制在仿真伺服系统中的应用 总被引:3,自引:1,他引:2
针对飞行仿真伺服系统动态性能要求的特殊性和系统本身的非线性 ,提出了自适应模型跟踪的有效控制方法。文章在探讨参考模型选取的基础上 ,推导出一种飞行仿真位置伺服系统的自适应模型跟踪算法 ,并将其用于某一飞行仿真伺服系统。实验表明 ,该算法使系统获得了优良的动态性能 ,尤其对改善系统的频率响应 ,拓宽系统频带具有很好的效果。最后给出了部分实验结果 相似文献
178.
Autonomous navigation of spacecrafts is a difficult task, however, which is a must in future deep space exploration. With multiple spacecrafts flying in space, this aim can be achieved by formation flying spacecraft (FFS) utilizing inverse time difference of arrival (ITDOA) and inverse difference Doppler (IDD) methods, which can locate the position of earth-station from one-way uplink signals in the FFS coordinate, and by way of conversion of coordinates, the position of FFS is achieved in earth-centered earth-fixed (ECEF) coordinate. The ability of neural network (NN) filter in navigation to extract position of spacecrafts from random measuring noise of signal arrival time and Doppler shift is studied with different radius of FFS and surveying parameters. The NN filter used by spacecraft group is new way of unidirectional autonomous navigation and is of high precision of hybrid navigation. 相似文献
179.
180.