首页 | 本学科首页   官方微博 | 高级检索  
文章检索
  按 检索   检索词:      
出版年份:   被引次数:   他引次数: 提示:输入*表示无穷大
  收费全文   644篇
  免费   66篇
  国内免费   27篇
航空   300篇
航天技术   188篇
综合类   21篇
航天   228篇
  2024年   4篇
  2023年   17篇
  2022年   20篇
  2021年   18篇
  2020年   15篇
  2019年   11篇
  2018年   11篇
  2017年   13篇
  2016年   15篇
  2015年   15篇
  2014年   20篇
  2013年   22篇
  2012年   37篇
  2011年   61篇
  2010年   15篇
  2009年   17篇
  2008年   30篇
  2007年   36篇
  2006年   28篇
  2005年   46篇
  2004年   23篇
  2003年   41篇
  2002年   21篇
  2001年   28篇
  2000年   23篇
  1999年   30篇
  1998年   19篇
  1997年   21篇
  1996年   15篇
  1995年   12篇
  1994年   11篇
  1993年   8篇
  1992年   7篇
  1991年   11篇
  1990年   4篇
  1989年   4篇
  1988年   5篇
  1987年   3篇
排序方式: 共有737条查询结果,搜索用时 898 毫秒
731.
《中国航空学报》2023,36(4):252-267
A common necessity for prior unsupervised domain adaptation methods that can improve the domain adaptation in unlabeled target domain dataset is access to source domain dataset and target domain dataset simultaneously. However, data privacy makes it not always possible to access source domain dataset and target domain dataset in actual industrial equipment simultaneously, especially for aviation component like Electro-Mechanical Actuator (EMA) whose dataset are often not shareable due to the data copyright and confidentiality. To address this problem, this paper proposes a source free unsupervised domain adaptation framework for EMA fault diagnosis. The proposed framework is a combination of feature network and classifier. Firstly, source domain datasets are only applied to train a source model. Secondly, the well-trained source model is transferred to target domain and classifier is frozen based on source domain hypothesis. Thirdly, nearest centroid filtering is introduced to filter the reliable pseudo labels for unlabeled target domain dataset, and finally, supervised learning and pseudo label clustering are applied to fine-tune the transferred model. In comparison with several traditional unsupervised domain adaptation methods, case studies based on low- and high-frequency monitoring signals on EMA indicate the effectiveness of the proposed method.  相似文献   
732.
《中国航空学报》2022,35(9):95-105
Internet of Things (IoT) can be conveniently deployed while empowering various applications, where the IoT nodes can form clusters to finish certain missions collectively. As energy-efficient operations are critical to prolong the lifetime of the energy-constrained IoT devices, the Unmanned Aerial Vehicle (UAV) can be dispatched to geographically approach the IoT clusters towards energy-efficient IoT transmissions. This paper intends to maximize the system energy efficiency by considering both the IoT transmission energy and UAV propulsion energy, where the UAV trajectory and IoT communication resources are jointly optimized. By applying large-system analysis and Dinkelbach method, the original fractional optimization is approximated and reformulated in the form of subtraction, and further a block coordinate descent framework is employed to update the UAV trajectory and IoT communication resources iteratively. Extensive simulation results are provided to corroborate the effectiveness of the proposed method.  相似文献   
733.
《中国航空学报》2023,36(8):298-312
Due to the portability and anti-interference ability, vision-based shipborne aircraft automatic landing systems have attracted the attention of researchers. In this paper, a Monocular Camera and Laser Range Finder (MC-LRF)-based pose measurement system is designed for shipborne aircraft automatic landing. First, the system represents the target ship using a set of sparse landmarks, and a two-stage model is adopted to detect landmarks on the target ship. The rough 6D pose is measured by solving a Perspective-n-Point problem. Then, once the rough pose is measured, a region-based pose refinement is used to continuously track the 6D pose in the subsequent image sequences. To address the low accuracy of monocular pose measurement in the depth direction, the designed system adopts a laser range finder to obtain an accurate range value. The measured rough pose is iteratively optimized using the accurate range measurement. Experimental results on synthetic and real images show that the system achieves robust and precise pose measurement of the target ship during automatic landing. The measurement means error is within 0.4° in rotation, and 0.2% in translation, meeting the requirements for automatic fixed-wing aircraft landing.Received 5 July 2022; revised 19 August 2022; accepted 27 September 2022.  相似文献   
734.
面对我国现代航天高密度发射的需求,精准高效的遥测参数装订与核对尤为重要。本文基于XTCE标准定义的遥测参数格式,构建了XTCE标准对遥测参数数据底座,实现遥测参数的统一标准、统一管理和统一平台。阐述了XTCE标准的结构、火箭遥测数据库的生成和数据底座的构造。实现了对大型火箭遥测参数的自动装订,大幅提高了工作效率。  相似文献   
735.
《中国航空学报》2023,36(8):247-257
As for unmanned aircraft, the knowledge of the aircraft performance is directly related with the navigation, guidance, and control system programming. Therefore, the measured data in each phase of the flight must be sufficiently precise to obtain a good characterization of aircraft. This article proposes new methods of sending information to ground, which make it possible to know the aircraft behavior accurately, and for this purpose, four contributions have been made for ALO (Avión Ligero de Observación, Spanish acronym for Light Observation Aircraft). Currently, the characterization is based on data obtained at ten samples per second, insufficient to acquire detailed knowledge of what happened during the whole flight of an aircraft. As a result of these contributions, many more samples per second of accelerations and angular velocities are obtained at the most critical moments of the flight, such as takeoff or landing. Among the improvements included are data compression techniques, providing references to locate the measured data in time and identifying labels of each parameter.  相似文献   
736.
Multi-fidelity Data Fusion(MDF) frameworks have emerged as a prominent approach to producing economical but accurate surrogate models for aerodynamic data modeling by integrating data with different fidelity levels. However, most existing MDF frameworks assume a uniform data structure between sampling data sources; thus, producing an accurate solution at the required level, for cases of non-uniform data structures is challenging. To address this challenge, an Adaptive Multi-fidelity Data Fusion(...  相似文献   
737.
障碍物数据集是国际民航组织在航空情报管理(AIM)体系下提出的一种基于航空信息交换模型(AIXM)规范的航空情报数据集,该数据集中障碍物的查询将直接影响机场净空评估与飞行程序设计。在分析障碍物数据集的时间与空间属性基础上,利用时空数据模型与航空信息交换模型规范,提出一种基于时间点和空间位置的障碍物数据集查询方法, 用于解决障碍物数据集的查询问题;构建障碍物查询与可视化系统,并通过设计随机实验和实例应用对该方法的可行性和可靠性进行验证。结果表明:该障碍物数据集查询方法能够提取出对机场净空与飞行程序设计有影响的障碍物,增强了飞行程序设计人员对机场障碍物分布的情景意识。  相似文献   
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号