全文获取类型
收费全文 | 5241篇 |
免费 | 800篇 |
国内免费 | 913篇 |
专业分类
航空 | 4053篇 |
航天技术 | 960篇 |
综合类 | 769篇 |
航天 | 1172篇 |
出版年
2024年 | 14篇 |
2023年 | 78篇 |
2022年 | 141篇 |
2021年 | 177篇 |
2020年 | 192篇 |
2019年 | 203篇 |
2018年 | 206篇 |
2017年 | 205篇 |
2016年 | 246篇 |
2015年 | 216篇 |
2014年 | 338篇 |
2013年 | 277篇 |
2012年 | 338篇 |
2011年 | 384篇 |
2010年 | 250篇 |
2009年 | 297篇 |
2008年 | 344篇 |
2007年 | 364篇 |
2006年 | 355篇 |
2005年 | 285篇 |
2004年 | 249篇 |
2003年 | 235篇 |
2002年 | 198篇 |
2001年 | 180篇 |
2000年 | 155篇 |
1999年 | 118篇 |
1998年 | 121篇 |
1997年 | 97篇 |
1996年 | 89篇 |
1995年 | 75篇 |
1994年 | 89篇 |
1993年 | 80篇 |
1992年 | 88篇 |
1991年 | 84篇 |
1990年 | 75篇 |
1989年 | 61篇 |
1988年 | 30篇 |
1987年 | 7篇 |
1986年 | 1篇 |
1985年 | 2篇 |
1984年 | 10篇 |
排序方式: 共有6954条查询结果,搜索用时 15 毫秒
91.
飞机飞行控制律/操纵效率器多学科优化设计 总被引:1,自引:1,他引:1
基于近似模型和遗传算法,针对多操纵面布局飞机提出一种对全包线飞行控制律和操纵效率器几何形状与位置进行多学科优化的设计方法.该方法采用力矩控制方式进行控制,应用鲁棒增益调参方法设计全包线飞行控制系统,利用试验设计方法和径向基神经网络响应面获取近似的气动学科模型和控制学科模型,在近似模型基础上由遗传算法获得优化的设计参数并最终获得优化的控制律和操纵效率器.以某多操纵面布局无尾飞机为例进行计算机飞行仿真验证,结果表明该方法具有可行性. 相似文献
92.
SUN Huixian WU Ji DAI Shuwu ZHAO Baochang SHU Rong CHANG Jin WANG Huanyu ZHANG Xiaohui REN Qiongying CHEN Xiaomin OUYANG Ziyuan ZOU Yongliao 《空间科学学报》2008,28(5)
Chang'E-1,the orbiter circling the moon 200km above the moon surface,is the first Chinese Lunar exploration satellite.The satellite was successfully launched on 24th October 2007.There are 8 kinds of scientific payloads onboard,including the stereo camera,the laser altimeter,the Sagnac-based interferometer image spectrometer,the Gamma ray spectrometer,the X-ray spectrom-eter,the microwave radiometer,the high energy particle detector,the solar wind plasma detector and a supporting payload data management system.Chang'E-1 opened her eyes to look at the moon and took the first batch of lunar pictures after her stereo camera was switched on in 20th November 2007.Henceforth all the instruments are successfully switched on one by one.After a period of parameter adjustment and initial check out,all scientific instruments are now in their normal operating phase.In this paper,the payloads and the initial observation results are introduced. 相似文献
93.
D. Maravilla B. Mendoza E. Juregui 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,42(9):1593-1600
Minimum extreme temperature series from several meteorological stations of the Gulf of Mexico are spectrally analyzed using the Maximum Entropy Method.We obtained significant periodicities similar to those found in meteorological and solar activity phenomena. This indicates that probably the solar activity signals are present in the minimum extreme temperature records of this Mexican region. 相似文献
94.
Ondřej Ploc Lembit Sihver Dmitry Kartashov Vyacheslav Shurshakov Raisa Tolochek 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
“Protective curtain” was the physical experiment onboard the International Space Station (ISS) aimed on radiation measurement of the dose – reducing effect of the additional shielding made of hygienic water-soaked wipes and towels placed on the wall in the crew cabin of the Service module Zvezda. The measurements were performed with 12 detector packages composed of thermoluminescent detectors (TLDs) and plastic nuclear track detectors (PNTDs) placed at the Protective curtain, so that they created pairs of shielded and unshielded detectors. 相似文献
95.
以四氯化碳为吸收液采集压缩气体中的油类物质,用红外光度法测定油含量,依据JJF 1059.1-2012《测量不确定度评定与表示》,评定了红外光度法测定压缩气体中油含量结果的不确定度。分析了影响不确定度的因素,对各不确定度分量进行了分析和计算,当压缩气体中油测量结果为5.52mg/m3时,扩展不确定度为0.68mg/m3。 相似文献
96.
组合卫星导航系统的快速选星方法 总被引:1,自引:1,他引:1
分析了选星数目与几何精度因子(GDOP, Geometry Dilution of Precision)及导航运算量的关系,基于遗传算法提出了一种以满足用户定位精度需求为条件的快速选星方法——快速遗传选星法.根据用户需求确定选星数目初值、选星数目最大值和GDOP阈值,构造选星方案的初始种群,在进化代数上限为1的条件下对种群进行选择、交叉和变异运算,获得初始选星解,根据初始解的GDOP与阈值的关系确定是否依据GDOP最小原则对初始解进行优化,直至满足算法终止条件,输出选星解.仿真结果表明,该算法可以在一次进化之内以不低于92.45%的概率满足GDOP阈值在2.5~6的要求,同时可有效降低54.75%以上的导航运算量. 相似文献
97.
Fridrich Valach Josef Bochníček Pavel Hejda Miloš Revallo 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
The paper deals with the relation of the southern orientation of the north–south component Bz of the interplanetary magnetic field to geomagnetic activity (GA) and subsequently a method is suggested of using the found facts to forecast potentially dangerous high GA. We have found that on a day with very high GA hourly averages of Bz with a negative sign occur at least 16 times in typical cases. Since it is very difficult to estimate the orientation of Bz in the immediate vicinity of the Earth one day or even a few days in advance, we have suggested using a neural-network model, which assumes the worse of the possibilities to forecast the danger of high GA – the dominant southern orientation of the interplanetary magnetic field. The input quantities of the proposed model were information about X-ray flares, type II and IV radio bursts as well as information about coronal mass ejections (CME). In comparing the GA forecasts with observations, we obtain values of the Hanssen–Kuiper skill score ranging from 0.463 to 0.727, which are usual values for similar forecasts of space weather. The proposed model provides forecasts of potentially dangerous high geomagnetic activity should the interplanetary CME (ICME), the originator of geomagnetic storms, hit the Earth under the most unfavorable configuration of cosmic magnetic fields. We cannot know in advance whether the unfavorable configuration is going to occur or not; we just know that it will occur with the probability of 31%. 相似文献
98.
99.
介绍了直流电阻仪器自动检测系统的组成、测量原理和检定方法以及系统实现的功能和特点 ,并进行了测量不确定度评定 相似文献
100.
介绍了控制系统在热值比较稳定的前提下,依靠控制加热炉排气中的残氧量以降低空燃比,达到降低排气热损失的目的,实现了加热炉节能降耗. 相似文献