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21.
复杂可修系统可信度建模对保证效能的定量分析至关重要.本文在考虑不同维修状况的基础上,着重对不同任务剖面内相应任务阶段中武器装备可信度进行了深入的定量分析和综合,进而构造出武器装备的可信度矩阵,用于武器装备的效能分析;文中以某地面车辆为例,进一步论证了武器装备可信度矩阵的工程含义,旨在为合理确定一大类武器装备的效能和可信度指标提供理论依据.  相似文献   
22.
A theoretical model of semi-elliptic surface crack growth based on the low cycle strain damage accumulation near the crack tip along the cracking direction and the Newman–Raju formula is developed. The crack is regarded as a sharp notch with a small curvature radius and the process zone is assumed to be the size of cyclic plastic zone. The modified Hutchinson, Rice and Rosengren(HRR) formulations are used in the presented study. Assuming that the shape of surface crack front is controlled by two critical points: the deepest point and the surface point.The theoretical model is applied to semi-elliptic surface cracked Al 7075-T6 alloy plate under cyclic loading, and five different initial crack shapes are discussed in present study. Good agreement between experimental and theoretical results is obtained.  相似文献   
23.
一种组合体航天器帆板的光照遮挡计算新方法   总被引:1,自引:0,他引:1  
提出了一种新的太阳帆板遮挡计算方法,用于组合体航天器的能量平衡分析与计算。根据航天器轴线与帆板转轴垂直的几何关系,将其沿轴线离散化为若干平面的集合,将所分析的帆板离散化为点集,判断离散点沿太阳矢量逆向是否经过离散的舱体平面或其它帆板平面,以此确定遮挡关系。通过仿真计算得到不同入射太阳方向下某组合体对应的遮挡区域,结果表明,新方法适用于轴对称形状组合体航天器的帆板遮挡分析。  相似文献   
24.
A new concept of spaceborne synthetic aperture radar (SAR) implementation has recently been proposed - the constellation of small spaceborne SAR systems. In this implementation, several formation-flying small satellites cooperate to perform multiple space missions. We investigate the possibility to produce high-resolution wide-area SAR images and fine ground moving-target indicator (GMTI) performance with constellation of small spaceborne SAR systems. In particular, we focus on the problems introduced by this particular SAR system, such as Doppler ambiguities, high sparseness of the satellite array, and array element errors. A space-time adaptive processing (STAP) approach combined with conventional SAR imaging algorithms is proposed which can solve these problems to some extent. The main idea of the approach is to use a STAP-based method to properly overcome the aliasing effect caused by the lower pulse-repetition frequency (PRF) and thereby retrieve the unambiguous azimuth wide (full) spectrum signals from the received echoes. Following this operation, conventional SAR data processing tools can be applied to focus the SAR images fully. The proposed approach can simultaneously achieve both high-resolution SAR mapping of wide ground scenes and GMTI with high efficiency. To obtain array element errors, an array auto-calibration technique is proposed to estimate them based on the angular and Doppler ambiguity analysis of the clutter echo. The optimizing of satellite formations is also analyzed, and a platform velocity/PRF criterion for array configurations is presented. An approach is given to make it possible that almost any given sparse array configuration can satisfy the criterion by slightly adjusting the PRF. Simulated results are presented to verify the effectiveness of the proposed approaches.  相似文献   
25.
包栗 《西南航空》2006,(1):74-76,78
眼前的折多山让人无法忍受,海拔4280米的垭口淹没在汽车尾气和鼎沸人声之中。有人在攀援佛塔,有人在抓扯风马旗,雪坡上满是豪气干云的征服者嘴脸.著名的康藏第一关正以它汉藏界山的博大胸怀接纳无知游人.没办浩.今天是伟大的五月一日,山洪般的旅游大潮从城市席卷而至,湮没郊野,淫没乡镇,湮没崇山峻岭,所及之处皆为沼国.  相似文献   
26.
一种摇臂式起落架的两种建模及结果对比   总被引:1,自引:0,他引:1  
为了满足适坠性能要求,一种摇臂式起落架采用了双腔缓冲器。本文详细推导了拉格朗日方程下该起落架的动力学方程,并编程数值计算了四种状态的着陆性能。同时在Adams/Aircraft平台下建立了该起落架模型,通过编写子程序的方法实现了该双腔缓冲器的功能扩展。Adams/Aircraft平台下的仿真结果与数值计算的结果吻合较好,为起落架性能分析提供了很好的相互验证方法。  相似文献   
27.
良好的居信环境不仅有利于身心健康,而且,对人类大脑智力的发育和发展提供了优良条件,现代科学研究表明:良好的环境可使人类大脑的思维效果提高15-35%。  相似文献   
28.
为了研究地球同步轨道量子密钥分发过程中星地量子信道特性,项目团队研制了搭载于实践二十卫星的极弱光偏振态分发设备,开展了地球同步轨道卫星与地面间光子偏振态的传输实验。实验时,星载偏振光分发设备根据遥控指令以50MHz频率驱动四个激光器出光,分发|0〉、|π/2〉、|π/4〉和|3π/4〉四种偏振态光子,经过长距离的空间传输后由地面站望远镜接收,最后由超导探测器探测。研究结果表明,地球同步轨道卫星到地面站的光学链路衰减约为100~110 dB,通道误码率约为2%~8%,满足量子密钥分发误码率的安全性要求。  相似文献   
29.
本文提出分别研究电池开路电压在充电结束后停置过程和放电结束后停置过程的不同变化规律,并考虑了不同停置时间在两个过程中的作用和影响,从而达到提高开路电压法估算荷电状态精度的效果。实验验证表明,此方法的精度比传统开路电压法更加准确。  相似文献   
30.
Civil aviation faces great challenges because of its robust projected future growth and potential adverse environmental effects. The classical Tube-And-Wing(TAW) configuration following the Cayley's design principles has been optimized to the architecture's limit, which can hardly satisfy the further requirements on green aviation. By past decades' investigations the BlendedWing-Body(BWB) concept has emerged as a potential solution, which can simultaneously fulfill metrics of noise, emission and fuel burn. The purpose of the present work is to analyze the developments of critical technologies for BWB conceptual design from a historical perspective of technology progress. It was found that the high aerodynamic efficiency of BWB aircraft can be well scaled by the mean aerodynamic chord and wetted aspect ratio, and should be realized with the trade-offs among stability and control and low-speed performance. The structure concepts of non-cylinder pressurized cabin are of high risks on weight prediction and weight penalty. A static stability criterion is recommended and further clear and adequate criteria are required by the evaluations of flying and handling qualities. The difficulties of propulsion and airframe integration are analyzed. The energy to revenue work ratios of well-developed BWB configurations are compared,which are 31.5% and 40% better than that of TAW, using state-of-art engine technology and future engine technology, respectively. Finally, further study aspects are advocated.  相似文献   
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