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   1004篇
  免费   108篇
  国内免费   446篇
航空   951篇
航天技术   298篇
综合类   203篇
航天   106篇
  2024年   1篇
  2023年   16篇
  2022年   18篇
  2021年   43篇
  2020年   35篇
  2019年   41篇
  2018年   50篇
  2017年   46篇
  2016年   62篇
  2015年   57篇
  2014年   63篇
  2013年   53篇
  2012年   71篇
  2011年   86篇
  2010年   65篇
  2009年   86篇
  2008年   86篇
  2007年   75篇
  2006年   62篇
  2005年   51篇
  2004年   40篇
  2003年   45篇
  2002年   39篇
  2001年   45篇
  2000年   33篇
  1999年   31篇
  1998年   40篇
  1997年   28篇
  1996年   27篇
  1995年   38篇
  1994年   48篇
  1993年   16篇
  1992年   13篇
  1991年   8篇
  1990年   11篇
  1989年   11篇
  1988年   14篇
  1987年   1篇
  1986年   2篇
  1984年   1篇
排序方式: 共有1558条查询结果,搜索用时 15 毫秒
921.
韦文书  荆武兴  高长生 《航空学报》2013,34(7):1520-1530
捕获非合作目标后航天器质量特性发生突变,这大大地增加了系统的不确定性,控制不当容易导致失稳.为避免控制过程中航天器出现较大系统干扰问题,提出了先识别捕获后的系统质量特性,而后合理摆放非合作目标的自主稳定策略.首先,对航天器捕获过程和自主稳定策略进行了描述;其次,依据动量矩定理建立了非合作目标与航天器组合系统的数学模型,推导了非合作目标位置与质量特性之间的关系;然后,基于航天器数学模型和姿态测量信息,采用非线性规划方法对质量特性进行了辨识;最后,利用滑模变结构理论设计了非合作目标的控制回路,采用Lyapunov理论对系统的稳定性进行了分析.仿真结果表明:本文提出的自主配平策略响应快、精度高,适合在轨服务.  相似文献   
922.
为了在液体火箭发动机试验过程中缩短低温气动阀的响应时间,减少非线性求解阀门动态响应的计算量,提升试验过程中的安全性与可靠性,根据低温气动阀的工作原理,构建阀门的动态响应非线性传递模型,并在此基础上,通过引入变步长系数与定义遗忘因子,在四阶龙格-库塔法基础上,构建了一种动态递推龙格-库塔法的非线性动力学求解方法,并提出响应速度的改进方案.最后通过实例的验证与仿真,为提升低温气动阀响应速度提供了一种方法指导,为提高液体火箭发动机试验技术提供了支持.  相似文献   
923.
《中国航空学报》2020,33(10):2499-2509
Common, unsteady aerodynamic modeling methods usually use wind tunnel test data from forced vibration tests to predict stable hysteresis loop. However, these methods ignore the initial unstable process of entering the hysteresis loop that exists in the actual maneuvering process of the aircraft. Here, an excitation input suitable for nonlinear system identification is introduced to model unsteady aerodynamic forces with any motion in the amplitude and frequency ranges based on the Least Squares Support Vector Machines (LS-SVMs). In the selection of the input form, avoiding the use of reduced frequency as a parameter makes the model more universal. After model training is completed, the method is applied to predict the lift coefficient, drag coefficient and pitching moment coefficient of the RAE2822 airfoil, in sine and sweep motions under the conditions of plunging and pitching at Mach number 0.8. The predicted results of the initial unstable process and the final stable process are in close agreement with the Computational Fluid Dynamics (CFD) data, demonstrating the feasibility of the model for nonlinear unsteady aerodynamics modeling and the effectiveness of the input design approach.  相似文献   
924.
Space weather forecasts are currently used in areas ranging from navigation and communication to electric power system operations. The relevant forecast horizons can range from as little as 24 h to several days. This paper analyzes the predictability of two major space weather measures using new time series methods, many of them derived from econometrics. The data sets are the Ap geomagnetic index and the solar radio flux at 10.7 cm. The methods tested include nonlinear regressions, neural networks, frequency domain algorithms, GARCH models (which utilize the residual variance), state transition models, and models that combine elements of several techniques. While combined models are complex, they can be programmed using modern statistical software. The data frequency is daily, and forecasting experiments are run over horizons ranging from 1 to 7 days. Two major conclusions stand out. First, the frequency domain method forecasts the Ap index more accurately than any time domain model, including both regressions and neural networks. This finding is very robust, and holds for all forecast horizons. Combining the frequency domain method with other techniques yields a further small improvement in accuracy. Second, the neural network forecasts the solar flux more accurately than any other method, although at short horizons (2 days or less) the regression and net yield similar results. The neural net does best when it includes measures of the long-term component in the data.  相似文献   
925.
Since 30 September 2009, following the launch and in-orbit testing of the most sophisticated gravity mission ever built, the European Space Agency (ESA) GOCE satellite is in ‘measurement mode’, providing continuous time series of satellite gravity gradient (SGG) observations and GPS satellite-to-satellite tracking (SST) observations. The availability of GPS SST observations allows the precise reconstruction of the GOCE position and thus the precise geolocation of the SGG observations. The SGG observations are based on the differences between observations taken by pairs of accelerometers, which need to be corrected first by applying a so-called calibration matrix and second by subtracting rotational terms (centrifugal and angular accelerations).  相似文献   
926.
辐射生物物理模型对于准确、有效地评估空间辐射引起的生物损伤及风险具有重要意义。目前较为流行的基于地基模拟的“靶效应模型”和“非靶效应模型”,是进一步探索空间辐射生物物理模型的基础。在考虑了辐射的非靶效应和机体复杂的修复过程的基础上,将传统理论中“击中”即“失活”的线性关系进行了推广,提出了基于否定算子的靶效应模型。通过对辐射钝感和敏感的两类细胞辐射实验中剂量与细胞存活率数据进行拟合发现,对于正常皮肤成纤维细胞的存活率数据,经典的靶学说与基于否定算子的改进靶效应模型都有较好的拟合效果;而对于人类胚胎肝细胞的存活率数据,基于否定算子的改进靶效应模型的拟合结果明显优于传统的靶学说模型。拟合结果中的模型参数值在人成纤维细胞和胚胎肝细胞中明显不同,说明了本模型的参数与传能线密度,细胞的种类、以及修复能力等物理和生物因素有关。  相似文献   
927.
The events that occurred after 2007 such as Chinese anti-satellite test, explosion of Briz-M upper stage, break up of cosmos-2421 and collision of cosmos-2251 with Iridium-33 satellites have completely changed the spatial density patterns in low earth orbits. This has increased the risk of collision between active satellites and debris created by them. Aftermath, the risk assessment of possible collisions called as conjunction analysis of working satellites from day to day has become more crucial. Spatial density models are useful in understanding the long-term likelihood of a collision in a particular region of space and helpful in pre-launch orbit planning. In this paper we present an algorithmic procedure for automatically estimating exact model parameters corresponding to the peak location and number of peaks using wavelets that will speed up the parameter estimation process for the models with peaks.  相似文献   
928.
The composition of the space radiation environment inside spacecrafts is modified by the interaction with shielding material, with equipment and even with the astronauts’ bodies. Accurate quantitative estimates of the effects of nuclear reactions are necessary, for example, for dose estimation and prediction of single-event-upset rates. To this end, it is necessary to construct predictive models for nuclear reactions, which usually consist of an intranuclear-cascade or quantum-molecular-dynamics stage, followed by a nuclear-de-excitation stage.  相似文献   
929.
Due to the compound structure of the medium and large portions of energy transferred, a seismic excitation in the oceanic or continental lithosphere disturbs all types of geophysical fields. To investigate the problem of electromagnetic (EM) disturbances in the atmosphere from the seismically activated lithosphere, we have formulated two mathematical models of interaction of fields of different physical nature resulting in arising of the low-frequency (from 0.1 to 10 Hz by amplitude of a few hundreds of pT) EM signals in the atmosphere. First we have considered the EM field generation in the moving oceanic lithosphere and then in the moving continental one. For both cases, the main physical principles and geological data were applied for formulation of the model and characteristics of the computed signals of different nature agree with measurements of other authors. On the basis of the 2D model of the seismo-hydro-EM-temperature interaction in the lithosphere–Ocean–atmosphere domain, a block-scheme of a multisensory vertically distributed (from a seafloor up to the ionosphere) tsunami precursors’ detection system is described. On the basis of the 3D model of the seismo-EM interaction in a lithosphere–atmosphere domain, we explain why Prof. Kopytenko (Inst. IZMIRAN of Russian Acad. Sci.) and co-authors were able to estimate location of the future seismic epicenter area from their magnetic field measurements in the atmosphere near the earth’s surface.  相似文献   
930.
Turbulence affects both combustion and NO formation. Fluctuation correlations are ideally used for quantitative analysis. From the instantaneous chemical reaction rate expression,ignoring the third-order correlation terms, the averaged reaction rate will have four terms, including the term of averaged-variable product, a concentration fluctuation correlation term, and temperature-concentration fluctuation correlation term. If the reaction-rate coefficient is denoted as K, the temperature fluctuation would be included in the K fluctuation. In order to quantitatively study the effect of turbulence on NO formation in methane-air swirling combustion, various turbulencechemistry models are tested. The magnitudes of various correlations and their effects on the time-averaged reaction rate are calculated and analyzed, and the simulation results are compared with the experimental measurement data. The results show that among various correlation moments, the correlation between the reaction-rate coefficient K fluctuation with the concentration fluctuation is most important and is a strong nonlinear term.  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