全文获取类型
收费全文 | 6062篇 |
免费 | 1026篇 |
国内免费 | 863篇 |
专业分类
航空 | 3973篇 |
航天技术 | 1940篇 |
综合类 | 637篇 |
航天 | 1401篇 |
出版年
2024年 | 27篇 |
2023年 | 126篇 |
2022年 | 181篇 |
2021年 | 290篇 |
2020年 | 313篇 |
2019年 | 422篇 |
2018年 | 561篇 |
2017年 | 429篇 |
2016年 | 376篇 |
2015年 | 337篇 |
2014年 | 302篇 |
2013年 | 314篇 |
2012年 | 417篇 |
2011年 | 495篇 |
2010年 | 331篇 |
2009年 | 303篇 |
2008年 | 360篇 |
2007年 | 365篇 |
2006年 | 389篇 |
2005年 | 287篇 |
2004年 | 222篇 |
2003年 | 172篇 |
2002年 | 122篇 |
2001年 | 130篇 |
2000年 | 102篇 |
1999年 | 82篇 |
1998年 | 95篇 |
1997年 | 70篇 |
1996年 | 62篇 |
1995年 | 66篇 |
1994年 | 79篇 |
1993年 | 28篇 |
1992年 | 29篇 |
1991年 | 18篇 |
1990年 | 15篇 |
1989年 | 17篇 |
1988年 | 9篇 |
1987年 | 5篇 |
1986年 | 1篇 |
1984年 | 1篇 |
1981年 | 1篇 |
排序方式: 共有7951条查询结果,搜索用时 106 毫秒
1.
2.
3.
Ayodeji Ashidi Joseph Ojo Adekunle Adediji Oludare Ajewole 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(5):1612-1622
Existing amplitude scintillation prediction models often perform less satisfactorily when deployed outside the regions where they were formulated. This necessitates the need to evaluate the performance of scintillation models developed in one region using data data from other regions while documenting their relative errors. Due to its variation with elevation angle, frequency, other link parameters and meteorological factors, we employed three years (January 2016 to December 2018) of concurrently measured satellite radio beacons and tropospheric weather parameters to develop a location-based amplitude scintillation prediction model over the Earth-space path of Akure (7.17oN, 5.18oE), South-western Nigeria. The satellite beacon measurement used Tektronix Y400 NetTek Analyzer at 1 s integration time while meteorological parameters, namely; temperature, pressure and relative humidity were measured using Davis Vantage Vue weather station at 1 min integration time. Comparative study of the model’s performance with nine (9) existing scintillation prediction models indicates that the best and worst performing models, in terms of root mean square error (RMSE), are the Statistical Temperature and Refractivity (STN) and direct physical and statistical prediction (DPSP) models with values 11.48 and 51.03 respectively. Also, worst month analysis indicates that April, with respective enhancement and fade values of 0.88 and 0.90 dB for 0.01% exceedance, is the overall worst calendar month for amplitude scintillation. 相似文献
4.
研究微小卫星综合电子系统的SiP技术实现方法。首先介绍微小卫星综合电子系统结构的组成和采用SiP技术的必要性,然后对综合电子系统进行功能模块划分,并对其通用扩展模块进行详细的SiP设计,包括抗辐照器件选型、原型验证、SiP原理图、基板管壳一体化设计、建模仿真、制造加工、实装测试验证等,通过SiP技术实现了一种星载综合电子系统中通用扩展SiP芯片产品,经过实际验证测试,在保证模块功能和性能的前提下,整体模块重量从230 g减轻到48 g,体积由180 mm?130 mm?17 mm减小到46 mm?46 mm?8 mm,很好地满足了星载功能模块小型化、轻量化设计需求。 相似文献
5.
6.
7.
《中国航空学报》2020,33(11):2907-2920
This paper investigates a time-varying anti-disturbance formation problem for a group of quadrotor aircrafts with time-varying uncertainties and a directed interaction topology. A novel Finite-Time Convergent Extended State Observer (FTCESO) based fully-distributed formation control scheme is proposed to enhance the disturbance rejection and the formation tracking performances for networked quadrotors. By adopting the hierarchical control strategy, the multi-quadrotor system is separated into two subsystems: the outer-loop cooperative subsystem and the inner-loop attitude subsystem. In the outer-loop subsystem, with the estimation of disturbing forces and uncertain dynamics from FTCESOs, an adaptive consensus theory based cooperative controller is exploited to ensure the multiple quadrotors form and maintain a time-varying pattern relying only on the positions of the neighboring aircrafts. In the inner-loop subsystem, the desired attitude generated by the cooperative control law is stably tracked under a FTCESO-based attitude controller in a finite time. Based on a detailed algorithm to specify the cooperative control protocol, the feasibility condition to achieve the time-varying anti-disturbance formation tracking is derived and the rigorous analysis of the whole closed-loop multi-quadrotor system is given. Some numerical examples are conducted to intuitively demonstrate the effectiveness and the improvements of the proposed control framework. 相似文献
8.
《中国航空学报》2020,33(10):2716-2727
In this paper, an Unmanned Aerial Vehicle (UAV) enabled Mobile Edge Computing (MEC) system is studied, in which UAV acts as server to offer computing offloading service to the Mobile Users (MUs) with limited computing capability and energy budget. We aim to minimize the total energy consumption of MUs by jointly optimizing the bit allocation for uplink, computing at the UAV and downlink, along with the UAV trajectory in a unified framework. To this end, a trajectory constraint model is employed to avoid sudden changes of velocity and acceleration during flying. Due to high-order information in use, we lead to a more reasonable nonconvex optimization problem than prior arts. An Alternating Direction Method of Multipliers (ADMM) method is introduced to solve the optimization problem, which is decomposed into a set of easy sub-problems, to meet the requirement on the efficiency in edge computing. Numerical results demonstrate that our approach leads a smoother UAV trajectory, significantly save the energy consumption for UAV during flying. 相似文献
9.
10.