全文获取类型
收费全文 | 83篇 |
免费 | 4篇 |
国内免费 | 17篇 |
专业分类
航空 | 58篇 |
航天技术 | 21篇 |
综合类 | 15篇 |
航天 | 10篇 |
出版年
2023年 | 9篇 |
2022年 | 4篇 |
2021年 | 14篇 |
2020年 | 10篇 |
2019年 | 4篇 |
2018年 | 2篇 |
2016年 | 1篇 |
2015年 | 1篇 |
2014年 | 3篇 |
2013年 | 11篇 |
2012年 | 4篇 |
2011年 | 4篇 |
2010年 | 3篇 |
2009年 | 4篇 |
2008年 | 1篇 |
2007年 | 2篇 |
2006年 | 4篇 |
2005年 | 3篇 |
2004年 | 4篇 |
2003年 | 1篇 |
2002年 | 1篇 |
2000年 | 1篇 |
1998年 | 2篇 |
1996年 | 1篇 |
1995年 | 1篇 |
1994年 | 1篇 |
1993年 | 2篇 |
1992年 | 1篇 |
1991年 | 2篇 |
1989年 | 1篇 |
1988年 | 1篇 |
1986年 | 1篇 |
排序方式: 共有104条查询结果,搜索用时 93 毫秒
21.
针对导弹控制系统结构复杂,信号线繁多,难以在故障诊断软件设计中实现诊断过程图形化实时显示的问题,提出了一种基于自定义组件开发故障诊断软件的方法.根据导弹控制系统的故障诊断流程及实时显示需要,对其结构进行了分析,抽象出了主要组成元素--信号通道和部件,由此提出了需要定义的相应组件.用Borland C Builder6.0开发环境进行了应用实践,证明使用这种方法可快速开发出能图形化实时显示故障诊断过程的导弹控制系统故障诊断软件,开发出的软件还具有运行稳定、修改升级方便等优点. 相似文献
22.
An adaptive integration surface for predicting transonic rotor noise in hovering and forward flights
In this paper, a new permeable adaptive integration surface is developed in order to evaluate transonic rotor noise in accordance with FW-H_pds equations(Ffowcs Williams-Hawkings equations with penetrable data surface). Firstly, a nonlinear near-field solution is computed on the basis of Navier-Stokes equations, which is developed on moving-embedded grid methodology.The solution calculated through the present CFD method is used as the input for acoustic calculations by FW-H_pds equations. Then, two criteria for constructing integration surfaces are established based on the analysis of the quadrupole source strength and the nonlinear characteristic.A new surface is determined adaptively by the pressure gradient or density in a given flowfield,eschewing the uncertainties associated with determining cylinder-shaped integration surfaces. For varying hover cases, transonic noises are simulated with new integration surfaces for a UH-1 model rotor. Furthermore, numerical results of the new integration surface derived from the density perturbation value conform better to experimental data than results derived from the pressure gradient.Finally, the integration surface given by jrqj being 0.1, which is an applicable criterion obtained from hover cases, is used to predict transonic rotor noise in forward flight. The computational accuracy of the new integration surface method has been validated in predicting transonic rotor noise of an AH-1 model rotor at different advance ratios. 相似文献
23.
近些年来,随着计算机图形学、计算几何和计算机辅助设计与制造技术的发展,双参数曲面和一般立体模型的隐线消去算法变得越来越重要。这是因为双参数曲面和一般立体模型能够描述更复杂的曲面模型,而非参数曲面却难以描述它们。 本文给出了双参数曲面和一般立体模型的两种隐藏线消去算法。该算法存贮量小,运行速度较快,易于加到已有的绘图程序中。本文还利用Dxy-880绘图仪给出了各种算法的实例。 相似文献
24.
讨论了一种基于窗口和面向对象的用户界面设计思想及方法,并详细描述了各种类的定义.在DOS环境下运用WatcomC++语言开发并在微机上运行,可以使用户方便地进行再开发工作。界面运用事件处理方式由窗口、弹出菜单、图标、按钮等组成,效果良好 相似文献
25.
26.
27.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(6):1573-1587
This paper explores two types of mathematical functions to fit single- and full-frequency waveform of spaceborne Global Navigation Satellite System-Reflectometry (GNSS-R), respectively. The metrics of the waveforms, such as the noise floor, peak magnitude, mid-point position of the leading edge, leading edge slope and trailing edge slope, can be derived from the parameters of the proposed models. Because the quality of the UK TDS-1 data is not at the level required by remote sensing mission, the waveforms buried in noise or from ice/land are removed by defining peak-to-mean ratio, cosine similarity of the waveform before wind speed are retrieved. The single-parameter retrieval models are developed by comparing the peak magnitude, leading edge slope and trailing edge slope derived from the parameters of the proposed models with in situ wind speed from the ASCAT scatterometer. To improve the retrieval accuracy, three types of multi-parameter observations based on the principle component analysis (PCA), minimum variance (MV) estimator and Back Propagation (BP) network are implemented. The results indicate that compared to the best results of the single-parameter observation, the approaches based on the principle component analysis and minimum variance could not significantly improve retrieval accuracy, however, the BP networks obtain improvement with the RMSE of 2.55 m/s and 2.53 m/s for single- and full-frequency waveform, respectively. 相似文献
28.
本文在介绍MB86R01的特点和功能的基础上,以飞机座舱显示系统中常见的姿态画面为例,设计并开发了基于MB86R01的图形显示平台.这种图形显示平台在未来飞机显示系统中具有广阔应用前景。 相似文献
29.
Lin Cheng Zhenbo Wang Fanghua Jiang Junfeng Li 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(3):1114-1123
In this study, an adaptive neural network control approach is proposed to achieve accurate and robust control of nonlinear systems with unknown dynamics, wherein the neural network is innovatively used to learn the inverse problem of system dynamics with guaranteed convergence. This study focuses on the following three contributions. First, the considered system is transformed into a multi-integrator system using an input–output linearization technique, and an extended state observation technique is used to identify the transformed states. Second, an iterative control learning algorithm is proposed to achieve the neural network training, and stability analysis is given to prove that the network’s predictions converge to ideal control inputs with guaranteed convergence. Third, an adaptive neural network controller is developed by combining the trained network and a proportional-integral controller, and the long-standing challenge of model-based methods for control determination of unknown dynamics is resolved. Simulation results of a virtual control mission and an aerospace altitude tracking mission are provided to substantiate the effectiveness of the proposed techniques and illustrate the adaptability and robustness of the proposed controller. 相似文献
30.