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基于高度分集的两波束米波雷达测高方法及其应用 总被引:1,自引:0,他引:1
米波雷达的波束较宽、由于地面反射引起波瓣分裂,通常只能估高而不能用来测高.针对这一难题本文提出一种基于高度分集的两波束米波雷达测高方法.该方法采用高度不同的两个天线,利用波瓣分裂情况及相互相位关系来测量目标高度.文章分析了此方法测高的精度及影响精度的一些因素.本测高方法已应用于某型雷达信号处理机中,并取得良好效果. 相似文献
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K. Patel Ashutosh K. Singh P. Subrahmanyam A.K. Singh 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
The presence and movement of plasma density fluctuations in the F-region of the ionosphere are studied by monitoring phase and amplitude of radio waves propagating through the region. In this paper, we have used weak scattering theory and assumed the plasma density fluctuations to behave like phase changing diffraction screen. Appropriate relations for scintillation index S4, and phase variance δ? are derived and computed for different parameters of the plasma density irregularities of the ionosphere. SROSS-C2 satellite in situ measurements of plasma density fluctuations, which provide direct information about the structure and morphology of irregularities that are responsible for scintillation of radio waves, were used first time to develop a scintillation model for low latitude. It is observed that the scintillation index S4 and phase variance δ? depends on the strength of the plasma turbulence. Finally, the results obtained from modeling are compared and discussed with the available recent results. 相似文献
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G. Uma P.S. Brahmanandam V.K.D. Srinivasu D.S.V.V.D. Prasad P.V.S. Rama Rao 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(7):1736-1743
In this research, it is presented the daytime amplitude scintillations recorded at VHF frequency (244 MHz) at an Indian low-latitude station, Waltair (17.7°N, 83.3°E) during seven continuous years (1997–2003). Contrary to the nighttime scintillation seasonal trends, the occurrence of daytime scintillations maximizes during summer followed by winter and the equinox seasons. The fade depths, scintillation indices and the patch durations of daytime scintillations are meager when compared with their nighttime counterparts. A co-located digital high frequency (HF) ionosonde radar confirms the presence of sporadic (Es) layers when daytime scintillations are observed. The presence of daytime scintillations is evident when the critical frequency of the Es-layer (foEs) is ≥4 MHz and Es-layers are characterized by a highly diffuse range spread Es echoes as can be seen on ionograms. It is surmised that the gradient drift instability (GDI) seems to be the possible mechanism for the generation of these daytime scintillations. It is quite likely that the spread Es-F-layer coupling is done through polarization electric fields (Ep) that develop inside the destabilized patches of sporadic E layers, which are mapped up to the F region along the field lines as to initiate the daytime scintillations through the GDI mechanism. Further, the presence of additional stratification of ionosphere F-layer, popularly known as the F3-layer, is observed on ionograms once the Es-layers and daytime scintillations are ceased. 相似文献
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Vaios Lappas Nasir Adeli Lourens Visagie Juan Fernandez Theodoros Theodorou Willem Steyn Matthew Perren 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
CubeSail is a nano-solar sail mission based on the 3U CubeSat standard, which is currently being designed and built at the Surrey Space Centre, University of Surrey. CubeSail will have a total mass of around 3 kg and will deploy a 5 × 5 m sail in low Earth orbit. The primary aim of the mission is to demonstrate the concept of solar sailing and end-of-life de-orbiting using the sail membrane as a drag-sail. The spacecraft will have a compact 3-axis stabilised attitude control system, which uses three magnetic torquers aligned with the spacecraft principle axis as well as a novel two-dimensional translation stage separating the spacecraft bus from the sail. CubeSail’s deployment mechanism consists of four novel booms and four-quadrant sail membranes. The proposed booms are made from tape-spring blades and will deploy the sail membrane from a 2U CubeSat standard structure. This paper presents a systems level overview of the CubeSat mission, focusing on the mission orbit and de-orbiting, in addition to the deployment, attitude control and the satellite bus. 相似文献
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PLL两点调制在GMSK调制器中的应用 总被引:1,自引:0,他引:1
分析了HDL数据链发信机设计中的几种GMSK调制方法;阐述了用PLL两点调制的必要性,进而给出了基于PLL的GMSK两点调制的模型。同时,对非线性模型进行线性化等效,列出它们的闭环传递函数,并通过Matlab仿真波形来观察频率响应曲线;最后对调制系统进行ADS仿真,分析系统的收敛性,通过时域、频域调制波形分析,得到最优系统参数。 相似文献
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蒋兰 《中国民航飞行学院学报》2009,20(5)
无线电干扰一直是困扰民航地空通信的一大难题.以2007年下半年贵州空管分局塔台主频受到广播电台干扰的排查过程为例,归纳总结出一些预防和查找民航VHF无线电干扰的方法. 相似文献
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针对VHF/UHF频段航天器舱体屏蔽处理难度大的问题,提出一种基于等效导纳模型的屏蔽效能分析方法。该方法将屏蔽舱体孔缝等效为波导结构,基于变分法原理建立水平电容和垂直电感模型,对参数失配和舱体厚度影响进行导纳匹配和孔缝宽度参数修正。采用传输线理论建立屏蔽效能分析数学模型。算例对比表明算法具有较高的分析精度,可有效分析孔缝不位于舱体中心位置和孔缝长度非波长整数倍时的屏蔽效能,并可准确预测舱体的谐振效应。将其应用到航天器舱体屏蔽效能分析中,对比结果表明算法可有效满足工程应用要求。 相似文献