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201.
CBERS-1卫星红外多光谱扫描仪图像预处理方法 总被引:1,自引:0,他引:1
文章介绍了中国和巴西联合研制的资源一号卫星 (CBERS_1)上的有效载荷之一 - -红外多光谱扫描仪 (IRMSS)图像数据的处理 ,包括错位校正、相对辐射校正和去除噪声等处理过程。 相似文献
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In order to promote an in-depth understanding of the mechanism of leading-edge flow separation control over an airfoil using a symmetrical Dielectric Barrier Discharge(DBD) plasma actuator excited by a steady-mode excitation, an experimental investigation of an SC(2)-0714 supercritical airfoil with a symmetrical DBD plasma actuator was performed in a closed chamber and a low-speed wind tunnel. The plasma actuator was mounted at the leading edge of the airfoil.Time-resolved Particle Image Velocimetry(PIV) results of the near-wall region in quiescent air suggested that the symmetrical DBD plasma actuator could induce some coherent structures in the separated shear layer, and these structures were linked to a dominant frequency of f0= 39 Hz when the peak-to-peak voltage of the plasma actuator was 9.8 kV. In addition, an analysis of flow structures without and with plasma actuation around the upper side of the airfoil at an angle of attack of18° for a wind speed of 3 m/s(Reynolds number Re = 20000) indicated that the dynamic process of leading-edge flow separation control over an airfoil could be divided into three stages. Initially, this plasma actuator could reinforce the shedding vortices in the separated shear layer. Then, these vortical structures could deflect the separated flow towards the wall by promoting the mixing between the outside flow with a high kinetic energy and the flow near the surface. After that, the plasma actuator induced a series of rolling vortices in the vicinity of the suction side of the airfoil, and these vortical structures could transfer momentum from the leading edge of the airfoil to the separated region, resulting in a reattachment of the separated flow around the airfoil. 相似文献
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《中国航空学报》2020,33(7):1877-1888
The air-cycle refrigeration system is widely used in commercial and military aircraft, and its efficiency greatly affects aircraft performance. Nowadays, this system requires a more efficient design and optimization method. In this paper, a short-cut optimization method with high efficiency and effectiveness is introduced for both conventional and electric air-cycle refrigeration systems. Based on the system characteristics, a four-layer parameter matching algorithm is designed which avoids computational difficulty caused by simultaneous equations. Fuel penalty is chosen as the objective function of optimization; design variables are reduced based on sensitivity analysis to improve optimization efficiency. The results show that the 3-variable optimization of the conventional air-cycle refrigeration system can obtain almost the same results as the traditional 6-variable optimization in that these two optimizations can both significantly reduce the fuel penalty. However, the computer running time of the 3-variable optimization is much shorter than that of the 6-variable optimization. The optimal fuel penalty of the electric air-cycle refrigeration system is lower than that of the conventional one. This study can provide reference for optimizing the air-cycle refrigeration system of aircraft. 相似文献
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基于自适应Siamese网络的无人机目标跟踪算法 总被引:1,自引:1,他引:1
无人机已被广泛应用到军事和民用领域,目标跟踪是无人机应用的关键技术之一。针对无人机跟踪过程中目标易发生形变、遮挡等问题,提出一种基于自适应Siamese网络的无人机目标跟踪算法。首先,利用2个卷积网络构建一个5层Siamese网络,通过对模板特征与当前帧图像特征进行卷积得到目标位置;其次,利用高斯混合模型对以往的预测结果进行建模并建立目标模板库;然后,从模板库中挑选出最可靠的目标模板并以此更新Siamese网络的匹配模板,使Siamese网络能够自适应目标的外观变化;最后,引入回归模型进一步精确目标位置,降低背景对网络性能的影响。仿真实验结果表明:该算法有效降低了形变、遮挡等情况对跟踪性能的影响,具有较高的准确率。 相似文献
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ANANALYSISOFPROPELLERLIFTING-LINETHEORYBYMATCHEDASYMPTOTICEXPANSIONSChenZemin;PanJieyuan;WuLiyi(InstituteofFluidMechanics,Bei... 相似文献