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Xuerui Wu Shuanggen Jin 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
Nowadays, GNSS-Reflectometry (GNSS-R) can be a new promising remote sensing tool in the ocean, snow/ice and land surfaces, e.g., vegetation biomass monitoring. Although GNSS-R provides a potentially special L-band multi-angular and multi-polarization measurement, the theoretical vegetation scattering properties and mechanisms for GNSS-R are not understood clearly. In this paper, the GNSS-R vegetation polarization scattering properties are studied and modeled at different incidence angles (specular direction). The bistatic scattering model Bi-mimics is employed, which is the first-order radiative transfer equation. As a kind of forest stand, the Aspen’s crown layer is composed of entire leaves, and its parameters in Mimics handbook are used as model input. The specular circular polarizations (co-polarization RR and cross-polarization LR) are simulated. For cross-polarization, the received polarization is assumed as a linear (horizontal and vertical) polarizations and ±45° linear polarizations. Therefore, the HR VR, +45R and −45R polarizations are simulated here. Contributions from different scattering components at RR, LR and VR polarization are also presented. For co-polarization, it is large in the whole specular angles (10–80°). The scattering trends of the other cross polarization (HR, LR, +45R and −45R) are a little similar when compared to the RR and RV. Therefore, the RHCP and V polarizations are more favorable to collect the reflected signals. The trunk heights and crown depths do not affect the scattering trends of RR, RV and RL, while the trunk height has some effect on the scattering amplitude of different polarizations. The azimuth angle has more effects on RR, RL and RV scattering, especially in lower than 50°. The observation angles and polarization combinations are extremely important for GNSS-R remote sensing. 相似文献
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依据热经济分析理论 ,并结合对飞机座舱盖热疲劳试验系统的运行模拟 ,找出了系统的关键能耗元件 ,针对它的热惯性是造成系统潜在高耗能的主要原因 ,提出了在关键能耗元件加隔热层的改进方案。对某型号座舱盖 100飞行小时试验 ,模拟计算结果的比较表明 ,改进方案能使试验能耗下降 37%。 相似文献
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基于CFD的软式空中加油锥套气动特性研究 总被引:1,自引:0,他引:1
无人机空中加油缺少人为的观测与控制,若要进行自主控制下的空中加油,获取精准的气动数据则十分关键。基于CFD研究了国外某型锥套的气动特性,通过改变锥套支撑臂数量、空速以及稳定伞面积3个因素,构建了不同的三维子模型。利用数值计算分析了其对锥套气动参数的影响,并探究了影响规律。仿真结果表明,支撑臂数量和稳定伞面积均会影响阻力系数,而空速对阻力系数几乎没有影响。该方法可以用来预测影响因素发生变化时锥套阻力系数的变化趋势,为分析锥套气动特性提供了理论依据。 相似文献
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预测座舱盖自由抛放运动轨迹方法的研究 总被引:1,自引:0,他引:1
系统地阐述了模拟气动力作用下物体运动过程的两类方法,即非定常数值模拟和气动系数法,并给出气动系数法中气动系数的三种获取手段。模拟对称座舱盖自由抛放过程的算例表明由于采用气动系数的不同,气动系数法会得到不同的计算结果,其中利用非定常气动系数得到的计算结果与非定常模拟预测值最为吻合。 相似文献
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不同透气情况降落伞的流场试验研究 总被引:1,自引:1,他引:1
降落伞由于其柔软透气性,其流场测量非常困难,而流场特性直接关系到降落伞的气动性能.本文采用风洞设备,利用七孔探针对不同透气情况下的降落伞的绕流流场进行了试验测量.采用Labview和Matlab engine混合编程技术进行七孔探针的压力数据采集和实时数据处理,获得了不同透气情况下伞衣周围的速度及压力分布情况,并对其进行了详细的流场分析.通过对不同透气伞流场的比较,可知透气情况对伞衣前后静压大小、尾流流线汇集位置、稳定性及噪音均有一定的影响.本文的研究解决了绕伞衣流场定量测量的难题,同时为降落伞的气动性能分析提供了一个很好的技术方案. 相似文献
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