全文获取类型
收费全文 | 887篇 |
免费 | 253篇 |
国内免费 | 147篇 |
专业分类
航空 | 641篇 |
航天技术 | 233篇 |
综合类 | 59篇 |
航天 | 354篇 |
出版年
2024年 | 4篇 |
2023年 | 27篇 |
2022年 | 66篇 |
2021年 | 50篇 |
2020年 | 47篇 |
2019年 | 49篇 |
2018年 | 46篇 |
2017年 | 24篇 |
2016年 | 35篇 |
2015年 | 36篇 |
2014年 | 45篇 |
2013年 | 39篇 |
2012年 | 40篇 |
2011年 | 65篇 |
2010年 | 48篇 |
2009年 | 22篇 |
2008年 | 37篇 |
2007年 | 52篇 |
2006年 | 62篇 |
2005年 | 44篇 |
2004年 | 46篇 |
2003年 | 42篇 |
2002年 | 26篇 |
2001年 | 34篇 |
2000年 | 41篇 |
1999年 | 39篇 |
1998年 | 38篇 |
1997年 | 34篇 |
1996年 | 28篇 |
1995年 | 18篇 |
1994年 | 24篇 |
1993年 | 21篇 |
1992年 | 19篇 |
1991年 | 10篇 |
1990年 | 9篇 |
1989年 | 7篇 |
1988年 | 5篇 |
1987年 | 8篇 |
排序方式: 共有1287条查询结果,搜索用时 31 毫秒
1.
Yi Wei Qingjun Li Fangnuan Xu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(1):393-400
A new orbit-attitude-vibration coupled dynamic model of the tethered solar power satellite (Tethered SPS) is established based on absolute nodal coordinate formulation. The Hamilton’s equation of the system is derived by introducing generalized momentum through Legendre transformation. The correctness of the proposed model is verified by an example. The dynamic characteristics of the Tethered SPS are studied using the symplectic Runge-Kutta method. Simulation results show that the orbital radius and the total energy of the system are well preserved. The attitude of the system is unstable when the mass of the bus system is small. However, the attitude stability is dependent on some other parameters of the system, which requires further studies. It is also found that the average tether force/deformation can be roughly estimated by simplifying the solar panel as a particle. The proposed model can be used to study the orbit-attitude-vibration coupled dynamics and control problems. 相似文献
2.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2023,71(7):3060-3075
Mega wildfires are one of the environmental disasters worldwide. This study evaluates the pre-fire species diversity and the indirect effects, including habitat loss for one of the largest wildfires in Manavgat (Antalya-Turkey) in 2021, with a two-step methodology. Here, (1) burnt areas in the Manavgat district (2021) were detected with remote sensing data from Sentinel-2A by delta Normalized Burn Ratio calculation for a selected area in Google Earth Engine, and (2) mammals' habitat vector data of International Union for Conservation of Nature (IUCN) Red List were integrated into Habitat and Biodiversity modelling of Terrset to analyze the alpha, beta, gamma diversity and Range Restriction Index for the wildfire region. In the total 4210 km2 study area, 696 km2 of the area was damaged by different fire severity; also, there were 56 mammal species' habitats here. These species include bats (i.e. Nyctalus leisleri), felids (i.e. Felis chaus), rodents (i.e. Rattus norvegicus) and large mammals (i.e. Ursus arctos). 88 % of these species are in IUCN's Least Concern category. The remaining classes are Near Threatened (3.7 %) and Vulnerable (7.4 %). This study also indicated that the burnt area's species richness does not totally consist of endemic species. Therefore, pre-fire species richness analyses of this study can be a base for further studies about the species' post-fire activity and occupancy.Furthermore, the 2021 mega wildfires show us the necessity of wildfire monitoring and risk studies in the entire Mediterranean ecosystem to evaluate the risks to the Sustainable Development Goals. Therefore, post-fire spatial data, fire migration monitorization, and recording of the species' activities should be performed temporally. In this way, the ability of wildlife's recovering, and the direct and indirect effects of the fire will be examined for ecosystems in the long term. 相似文献
3.
利用CHAMP卫星数据,对2002-2008年12个不同强度磁暴事件期间的热层大气密度变化特征进行分析,并研究对应磁暴期间大气模式NRLMSISE-00分布特征.结果表明,大磁暴期间日侧大气密度峰值从高纬到低纬的时间延迟为2h,中小磁暴期间的延迟时间为3~4h;春秋季暴时大气密度分布基本呈南北对称分布,而夏冬季大气密度的分布是夏半球大于冬半球,春秋季暴时大气密度大于夏冬季;NRLMSISE-00大气模式得到的热层大气密度很好的体现了半球分布以及季节分布的特征,但模式模拟结果偏小;Dst指数峰值比ap指数峰值更能反应大气密度的变化情况. 相似文献
4.
对一种抽展式火星车转移坡道开展柔顺性优化设计和动力学分析。首先,分析火星车与存在异面角的坡道的挤压几何原理。然后,设计坡道的间隙机构和限位机构,并计算出机构关键设计参数的最优值,以自适应调整两侧坡道的距离,〖JP2〗减小火星车与坡道护栏之间的相互作用力。最后,对坡道下落过程和火星车在坡道上的行驶过程进行动力学仿真,验证坡道柔顺性优化设计的效果。结果表明:优化后的坡道柔顺性大幅提高,坡道可以自适应调整两侧的距离;使用优化后的坡道,可以有效降低火星车与坡道护栏的作用力,实现火星车在坡道上的安全行驶。 相似文献
5.
A new modeling scheme for powered parafoil unmanned aerial vehicle platforms: Theory and experiments
《中国航空学报》2019,32(11):2466-2479
A novel framework is established for accurate modeling of Powered Parafoil Unmanned Aerial Vehicle (PPUAV). The model is developed in the following three steps: obtaining a linear dynamic model, simplifying the model structure, and estimating the model mismatch due to model variance and external disturbance factors. First, a six degree-of-freedom linear model, or the structured model, is obtained through dynamic establishment and linearization. Second, the data correlation analysis is adopted to determine the criterion for proper model complexity and to simplify the structured model. Next, an active model is established, combining the simplified model with the model mismatch estimator. An adapted Kalman filter is utilized for the real-time estimation of states and model mismatch. We finally derive a linear system model while taking into account of model variance and external disturbance. Actual flight tests verify the effectiveness of our active model in different flight scenarios. 相似文献
6.
针对复杂动态环境下无人飞行器的动态障碍规避问题,基于合理假设建立了无人飞行器和动态障碍的运动学模型,并综合考虑无人飞行器飞行过程中的终端约束、控制输入约束、安全避障约束等,以能量最少为性能指标构建动态避障问题数学描述。之后,针对终端约束和控制输入约束,依据优化模型预测静态规划算法(OMPSP)生成初始轨迹;针对动态避障问题的不等式约束,引入松弛变量并结合滑模变结构控制方法设计松弛变量动力学,实现对一个、多个或同时多个动态障碍的安全规避;最后,依据有限时间微分动态规划(RHDDP)算法进行轨迹优化,获得满足上述各种约束并能规避动态障碍的近似最优轨迹。 相似文献
7.
8.
针对飞机装配车间传统“领料式”物料配送存在的弊端,提出了一种工艺模型驱动的物料动态精准配送方法,构建了飞机装配车间物料精准配送管理系统,阐述了系统构建涉及的关键技术难点,采用基于模型的三维可视化消耗式BOM重构方式,建立与设计了模型动态同步精准的MBOM工艺模型,利用RFID技术的优点实时获取物料信息,通过iGPS系统引导AGV物料运输平台来实现装配站位物料的高精度配送。 相似文献
9.
10.
旋转机构是旋转调制捷联惯导系统的关键部件之一。为了精确模拟旋转机构的动力学特性,研究了支撑旋转轴系的双列球轴承的动力学建模方法,提出了使用Bushing单元来建立同时具有径向移动刚度、轴向移动刚度和径向角刚度的三向刚度轴承动力学模型的方法。利用有限元数值仿真方法计算了三向刚度数值,并利用轴承手册上的经验公式进行了验证。在此基础上,建立了含弹性轴承支撑的旋转调制捷联惯导系统旋转机构的结构动力学有限元模型,分析比较了轴承有无角刚度两种状态下的固有模态。分析结果表明:对于旋转调制捷联惯导系统旋转机构来说,轴承模型角刚度对计算精度的影响较大,角刚度已知的模型更接近真实情况。 相似文献