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661.
    
The ionospheric error affects the accuracy of the Global Navigation Satellite Systems observation and precise orbit determination. Usually, only the first order ionospheric error is considered, which can be eliminated by the ionospheric-free linear combination observation. But the remaining higher order ionospheric error will affect the accuracy of observations and their applications. In this paper, the influence of the higher order ionospheric error have been studied by using the International Geomagnetic Reference Field 13 and the Global Ionosphere Maps model produced by the Center for Orbit Determination in Europe. Focus on ionospheric error, the experiment of paper at doy 302 in 2019, which show that the second order ionospheric error impacting BeiDou Navigation Satellite System (BDS) B1I and B3I observation is 6.3569 mm and 11.8484 mm, respectively. Whereas, the third order ionospheric error impacting BDS B1I and B3I observation is 0.1734 mm and 0.3977 mm, respectively. Due to the current measurement accuracy of BDS carrier-phase observation can reach 2 mm, the influence of high order ionospheric error on observation should be considered. For BDS precise orbit determination, the orbit overlapping results are indicated that its orbit accuracy can be improved approximately 5 mm with the higher order ionospheric error correction, which is also in agreement with the results of Satellite Laser Ranging in this work.  相似文献   
662.
    
《中国航空学报》2016,(2):403-410
An integrated design concept for crashworthy fuselage using sine-wave beam and strut is proposed and investigated. The finite element model of aircraft fuselage is built first. The structures above cabin floor, occupant and seat are simplified as two rigid blocks. The fuselage frame is redesigned, and the sine-wave beam is arranged under the frame. The impact dynamic performance of the aircraft with bottom sine-wave beam structure is studied and compared with that of conventional type. To obtain better crashworthiness performance, different rigidity of strut is combined with the sine-wave beam bottom structure. Numerical simulation result shows that the proposed sine-wave beam bottom structure could not only dissipate more proportion of impact kinetic energy but also reduce the initial peak acceleration. The structure and rigidity of strut have great influence on the crashworthiness performance. To give a better fuselage structure, both of the strut and bottom structure should be properly integrated and designed.  相似文献   
663.
从实际应用出发,论述了光切法应用于曲面数据采样的原理及方法;对采样数据的预处理技术进行了简要总结,详细讨论了点云数据的精简,提出采用简化多边形来精简点云数据的方法;并说明在Geomagic环境下进行数据精简以及曲面重构技术的应用,证明了该方法的有效性.  相似文献   
664.
Airborne synthetic aperture radar (SAR) has the capability of high-resolution, and spaceborne SAR has the capability of wide-swath. Inspired by recent advances in near-space defined as the region between 20 km and 100 km, this paper conceptually designed near-space vehicle-borne SAR. The near-space vehicle-borne SAR has the synthetical advantages of the satellite and airplane platforms. By placing SAR transmitter or receiver in near-space vehicles, many functions that are currently performed with satellites or airplanes could be performed in low cost way. These advantages make simultaneous high-resolution and wide-swath SAR imaging possible. As such, this paper focuses on the role of near-space vehicle for high-resolution and wide-swath SAR imaging, and deals with conceptual performance, as opposed to technological implementation. The concepts, models and processing algorithms are provided. To further suppress the azimuth ambiguities and extend swath width, multiple beams in azimuth is applied. Furthermore, an example near-space vehicle-borne SAR is designed. It is shown that the use of cost effective near-space vehicles can provide the solutions that were previously thought to be out of reach for remote sensing scientists and customers.  相似文献   
665.
    
Interaction of a powerful obliquely incident wave beam of decameter radio waves with the ionospheric F2 layer is analyzed. Much like the linear case, propagation through the natural anti-waveguide layer F2 splits the initial beam. Some part of its energy leaks through the ionospheric layer, the other part goes back along a downward trajectory. However, nonlinearity leads to further stratification of the ionospheric layer. A new feature, in comparison with the linear case, is appearing a narrow waveguide beneath the F2 layer maximum which traps a small part of the beam energy. We study the relationship between these parts of the wave field in a simplified model of parabolic F2 layer, with nonlinearity caused by thermal plasma expulsion from the high field intensity region. Analytical results are supplemented with numerical estimates of the effects.  相似文献   
666.
定向能武器及其应用   总被引:5,自引:0,他引:5  
介绍了未来战争中的一种重要武器———定向能武器,包括激光武器、粒子束武器和射频武器。概述了这三种武器的工作机理、主要特点并进行了相互比较,介绍了定向能武器的应用。  相似文献   
667.
基于相关运算的LIDAR测风速   总被引:5,自引:0,他引:5  
风速测量是激光雷达的应用之一。文中详细讨论了利用相关算法处理激光雷达采集的大气气溶胶回波信号计算风速的方法。介绍大气气溶胶回波信号的前处理,推演便于计算机处理的相关运算计算风速公式,运用Matlab 语言实现信号预处理及风速计算,给出实验结果并与香港天文台数据作比较分析,指出该方法的优点及局限性  相似文献   
668.
运用折射率匹配 (Refractive IndexMatching)技术 ,使混浊液内部自然对流的可视化图像速度测量成为可能。但由于来自微粒子的散乱光的影响 ,所得到的速度场出现了少量的误对应现象。为了解决这个问题 ,开发了新的可视化实验组合技术———折射率匹配与激光诱导荧光法 (LIF :Laser InducedFluorescence)组合 ,利用不同种类的粒子发光波长不同的特性 ,有效地去除了微粒子的散乱光 ,获得了清晰的示踪粒子的图像。笔者将简要介绍激光诱导荧光法的工作原理及其实验结果。  相似文献   
669.
很多人对液体粒子场的测量十分感兴趣,并且已有人进行了这方面的研究,但是对于液体颗粒的直径,粒子空间分布,很少有人得到较理想的结果。本文将介绍以下内容:(1)用全息术测量液体粒子场原理;(2)同轴远场拍摄光路; (3)同轴再现光路;(4)粒子场信息处理方法;(5)测量结果。最终的测量结果表明,用激光全息方法测量动态液体粒子场中的粒子直径、粒子空间分布具有迅速、准确、非接触之优点,用这一方法可以得到令人满意的结果。  相似文献   
670.
Dy对EB-PVDβ-NiAl涂层高温瞬态氧化行为的影响(英文)   总被引:1,自引:0,他引:1  
β-NiAl是一种有前景的应用于1150°C以上的抗氧化涂层材料。本文利用电子束物理气相沉积(EB-PVD)方法制备了0~0.5at%Dy含量的β-NiAl涂层,研究了涂层的瞬态氧化行为。1200°C时,在0.05at%Dy掺杂的涂层中只观察到了稳态α-Al2O3相,而在0.5at%Dy掺杂的涂层中,1h氧化过程中,发生了θ-Al2O3到α-Al2O3的相变。1100°C时,在最初的15min所有涂层均发生了θ-α相变。0.05at%Dy掺杂的涂层在45min的时候相变已经完成,这比0.5at%Dy掺杂涂层要早得多。过量Dy的掺杂能够延缓θ-α相变。未掺杂和过量掺杂涂层在20h氧化之后仍存在针状相θ-Al2O3,而0.05at%Dy掺杂的涂层中则为经典的颗粒状α-Al2O3形貌。  相似文献   
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