全文获取类型
收费全文 | 970篇 |
免费 | 242篇 |
国内免费 | 236篇 |
专业分类
航空 | 969篇 |
航天技术 | 163篇 |
综合类 | 121篇 |
航天 | 195篇 |
出版年
2024年 | 4篇 |
2023年 | 19篇 |
2022年 | 45篇 |
2021年 | 39篇 |
2020年 | 78篇 |
2019年 | 66篇 |
2018年 | 58篇 |
2017年 | 62篇 |
2016年 | 75篇 |
2015年 | 77篇 |
2014年 | 83篇 |
2013年 | 73篇 |
2012年 | 75篇 |
2011年 | 89篇 |
2010年 | 60篇 |
2009年 | 75篇 |
2008年 | 54篇 |
2007年 | 55篇 |
2006年 | 45篇 |
2005年 | 37篇 |
2004年 | 23篇 |
2003年 | 32篇 |
2002年 | 28篇 |
2001年 | 28篇 |
2000年 | 23篇 |
1999年 | 24篇 |
1998年 | 18篇 |
1997年 | 15篇 |
1996年 | 9篇 |
1995年 | 12篇 |
1994年 | 13篇 |
1993年 | 8篇 |
1992年 | 9篇 |
1991年 | 12篇 |
1990年 | 7篇 |
1989年 | 6篇 |
1988年 | 11篇 |
1986年 | 1篇 |
排序方式: 共有1448条查询结果,搜索用时 420 毫秒
871.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2020,65(1):470-480
Lodging is a common phenomenon in maize production, which seriously affects its yield, quality, and mechanical harvesting capacity. With good penetrating power, satellite radar can monitor crop growth even under cloudy weather conditions. In this study, a method based on the change in plant height before and after lodging in maize is proposed to calculate the lodging angle and monitor the lodging degree by using dual-polarization Sentinel-1A data. The results show that the optimal sensitive polarization combinations of maize plant height before and after lodging are VH/VV and VV, respectively. The lodging angle is calculated using the plant height inversion results before and after lodging. The overall accuracy of classifying lodging grade of maize is 67%. The proposed model based on lodging angle could effectively mapped the maize lodging range on a regional scale and classify the lodging grades. 相似文献
872.
《中国航空学报》2020,33(7):1980-1990
Uncontained Engine Rotor Failure (UERF) can cause a catastrophic failure of an aircraft, and the quantitative assessment of the hazards related to UERF is a very important part of safety analysis. However, the procedure for hazard quantification of UERF recommended by the Federal Aviation Administration in advisory circular AC20-128A is cumbersome, as it involves building auxiliary lines and curve projections. To improve the efficiency and general applicability of the risk angle calculation, a boundary discretization method is developed that involves discretizing the geometry of the target part/structure into node points and calculating the risk angles numerically by iterating a particular algorithm over each node point. The improved efficiency and excellent accuracy for the developed algorithm was validated through a comparison with manual solutions for the hazard quantification of the engine nacelle structures of a passenger aircraft using the guidance in AC20-128A. To further demonstrate the applicability of the boundary discretization method, the proposed algorithm was used to examine the influence of the target size and the distance between the target and rotor on the hazard probability. 相似文献
873.
Samy A. Khalil A.M. Shaffie 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
The hourly and daily measured clear-sky global solar radiation (G) and biologically important effective erythematic radiation (EER) incident on a horizontal surface at Cairo, Egypt (latitude 30° 05′ N & Longitude 31° 15′ E), during the period from January 1995 to December 2005 are used in this paper. The relationship between daily integrated totals of EER and the daily totals of broadband global solar radiation (250–2800 nm) is established. The temporal variability of the percentage ratio of the total daily erythema to total daily broadband solar global irradiation (EER/G) is determined. The monthly and the seasonal averages of the extraterrestrial UVB solar radiation, Mesurad and estímated UVB solar radiation and clearness index KtUVB of UVB radiation are discussed. The average monthly mean variation of slant ozone (Z) and UVB transmission (KtUVB) at the present work are found. The two variables show an opposite seasonal behavior, and the average monthly of slant ozone column and UVB transmission values shows the relationship between them in a clearer way than those of daily values. The estimated values of UVB solar radiation a good agreement with the measured values of the UVB solar radiation, the difference between the estimated and measured values of UVB solar radiation varies from 1.2% to 2.8%. The effect of the annual cycles of solar zenith angle (SZA) and total column ozone (TCO) on the ratios (EER/G) are presented and the correction factors are determined for removal of the ozone cycle. The seasonal variability of EER/G is also discussed. The effect of the annual cycles of solar zenith angle (SZA) and total column ozone (TCO) on the ratios (EER/G) is presented and the correction factors are determined for removal of the ozone cycle. 相似文献
874.
C.L. Liu G. Kirchengast K.F. Zhang R. Norman Y. Li S.C. Zhang B. Carter J. Fritzer M. Schwaerz S.L. Choy S.Q. Wu Z.X. Tan 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
Global Navigation Satellite System (GNSS) radio occultation (RO) is an innovative meteorological remote sensing technique for measuring atmospheric parameters such as refractivity, temperature, water vapour and pressure for the improvement of numerical weather prediction (NWP) and global climate monitoring (GCM). GNSS RO has many unique characteristics including global coverage, long-term stability of observations, as well as high accuracy and high vertical resolution of the derived atmospheric profiles. One of the main error sources in GNSS RO observations that significantly affect the accuracy of the derived atmospheric parameters in the stratosphere is the ionospheric error. In order to mitigate the effect of this error, the linear ionospheric correction approach for dual-frequency GNSS RO observations is commonly used. However, the residual ionospheric errors (RIEs) can be still significant, especially when large ionospheric disturbances occur and prevail such as during the periods of active space weather. In this study, the RIEs were investigated under different local time, propagation direction and solar activity conditions and their effects on RO bending angles are characterised using end-to-end simulations. A three-step simulation study was designed to investigate the characteristics of the RIEs through comparing the bending angles with and without the effects of the RIEs. This research forms an important step forward in improving the accuracy of the atmospheric profiles derived from the GNSS RO technique. 相似文献
875.
考虑末制导阶段捷联导引头视场角限制及攻击角度约束,提出一种基于三维比例导引攻击角度控制的导引律。首先,利用三维矢量制导模型和四元数理论实现三维比例导引的攻击角度预测,进而基于空间几何原理设计一种能够满足视场角约束的三维比例导引攻击角度控制方法。对闭环制导动力学进行分析,并采用李雅普诺夫原理证明视场角受限情况下的制导误差收敛性。分析该制导方法在导弹速度大小变化情况下的轨迹不变性,进而保证制导方法在速度大小变化情况下的有效性。理论分析和仿真校验结果说明了该方法的正确性和有效性。提出的方法可为视场角受限下的攻击角度控制导引律设计提供参考。 相似文献
876.
《中国航空学报》2020,33(2):493-500
Morphing wings can improve aircraft performance during different flight phases. Recently research has focused on steady aerodynamic characteristics of the morphing wing with a flexible trailing-edge, and the unsteady aerodynamic and stall characteristics in the deflection process of the morphing wing are worthy further investigation. The effects of the angle of attack and deflection rate on aerodynamic characteristics were examined, and based on the aerodynamic characteristics of the morphing wing, a method was developed to delay stall by using the flexible periodic trailing-edge deflection. The numerical results show that the lift coefficients in the deflection process are smaller than those in the static situation at small angles of attack, and that the higher the deflection rate is, the smaller the lift coefficients will be. On the contrary, at large angles of attack, the lift coefficients are higher than those in the static case, and they become larger with the increase of the deflection rate. Further, the periodic deflection of the flexible trailing-edge with a small deflection amplitude and high deflection rate can increase lift coefficients at the critical stall angle. 相似文献
877.
赵乃虎 《西安航空技术高等专科学校学报》2011,29(3):79-80
研究椭圆、双曲线、抛物线上三点构成直角三角形的充要条件,得到若干有益的结果。 相似文献
878.
879.
《中国航空学报》2021,34(2):240-251
This paper proposes a new three-dimensional optimal guidance law for impact time control with seeker’s Field-of-View (FOV) constraint to intercept a stationary target. The proposed guidance law is devised in conjunction with the concept of biased Proportional Navigation Guidance (PNG). The guidance law developed leverages a nonlinear function to ensure the boundedness of velocity lead angle to cater to the seeker’s FOV limit. It is proven that the impact time error is nullified in a finite-time under the proposed method. Additionally, the optimality of the biased command is theoretically analyzed. Numerical simulations confirm the superiority of the proposed method and validate the analytic findings. 相似文献
880.