共查询到20条相似文献,搜索用时 156 毫秒
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现有的技术较难满足星载多波束相控阵天线射频前端的通道间距,已有的研究工作大量集中在提高射频电路和芯片的集成度,提出采用稀疏布阵的方式来增加天线单元的平均间距,从而缓解现有技术条件下的高密度集成难题。设计了Ka频段八波束相控阵天线的稀疏布阵阵面,首先采用遗传算法优化设计64元稀疏子阵,子阵增益在±60°扫描范围内大于18.6dB,该子阵沿4个象限镜像对称,便于高效设计将不规则分布的天线单元端口与规则排布的R组件端口进行互连的带状线转接板,然后随机旋转、平移36个子阵拼接成全阵,在一定程度上打乱子阵分布均匀性,以起到栅瓣抑制的作用。该方法具有简单、高效、快捷的优点,稀疏阵列的设计结果基本能满足工程应用需求,适用于星载多波束相控阵。 相似文献
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为使阵列天线获得圆对称方向图,通常采用环阵的排列方式。文章研究了六边形环阵列天线的特殊方向图综合方法。文中采用非线性最小二乘法对影响天线方向图的诸多参数,如单元的幅度和相位、单元间距以及单元在阵中的位置等,进行了优化设计,以使阵列方向图在最小二乘意义上逼近预先给定的理想方向图。仿真结果表明该方法可行、有效。 相似文献
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文章基于多旋转关节空间太阳能电站(MR-SPS)方案,以降低远距离高压电力传输技术难度为核心,提出一种更新的模块化多旋转关节空间太阳能电站概念。该方案在分布式太阳电池分阵和多导电旋转关节基础上,对于微波发射天线阵也进行了模块化设计和分布式布局,实现了太阳电池分阵和微波发射天线分阵的一一对应,形成多个独立的太阳能发电与能量传输模块,通过模块的扩展实现整个空间太阳能电站。该方案大幅简化了空间电力传输与管理的复杂性和在轨组装的难度。同时各个模块完全独立,组装后即可单独工作,也提高了系统的可靠性。 相似文献
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Study on Multi-Rotary Joints Space Power Satellite Concept 总被引:1,自引:0,他引:1
The Space Power Satellite(SPS) would be a huge spacecraft capturing the power of solar radiation in space and to supply electric power to the electric grid on the ground. The SPS concept was proposed by Dr. Peter Glaser in 1968. SPS have been studied now for exactly fifty years by many scientists in various countries. It has been regarded as one of the most promising energy projects of the future and has been attracting more attention in recent years. More and more Chinese scholars and experts are paying attention to the development of SPS. Due to the huge size, immense mass and high power of such a satellite system, there are many technical difficulties which exist to realize SPS. In this paper, recent SPS research and development activities are reviewed first. Various SPS concepts are analyzed and compared. The primary scheme of the Multi-Rotary joint SPS(MR-SPS) is described. The main feature is that the huge solar array comprising many separate small solar sub-arrays and each solar sub-array has two middle power rotary joints. So, the most challenging technology, the high-power rotary joint, is simplified by using many middlepower rotary joints hence the possibility of a single-point failure of a single rotary joint is avoided. This enables easy assembly of the modular solar arrays. Finally some key technologies of MR-SPS are analyzed. 相似文献
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针对卫星导航信号参数估计性能严重影响导航定位精度,提出了一种利用电磁偶极子对提高信号波达方向和极化参数估计性能的方法。充分利用接收数据协方差矩阵,通过两次特征分解,由特征分解的特征值进行极化参数估计。利用小圆环子阵导向矢量得到波达方向的粗略而无模糊的估计,大圆环子阵导向矢量得到有模糊的估计,通过解模糊得到精确的无模糊的估计,从而大幅提高了到达角的估计精度。比较了单个圆环阵列和同心圆环阵列的参数估计性能,分析了参数估计精度对抗干扰性能的影响,仿真结果表明参数估计精度的提高有效改善了卫星导航抗干扰的性能。 相似文献
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针对一个基于四位数字移相器的相控阵天线试验子阵,对其进行波束指向性能分析,得到扫描波束的波束宽度、指向误差和增益跌落等参数,计算数据与试验结果基本吻合,该分析方法将可应用于更大规模相控阵天线的性能分析。 相似文献
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针对基于偶数(2q)阶累积量的测向算法中测向性能提高有限的问题,提出了一种基于多级嵌套 L 型阵列的2维测向算法。首先利用阵列的多级嵌套结构和2q阶累积量,形成具有更多自由度的虚拟均匀面阵;然后使用2维平滑方法,恢复其2q阶累积量矩阵的秩; 采用2维MUSIC算法,进行方位角和俯仰角的估计。与常规的2q MUSIC 算法相比,所提算法不仅具有更好的测向精度,而且由于虚拟均匀阵包含更多的虚拟阵元,因此能够估计更多信源的方位角。另外,针对该L型阵列的最优配置问题,推导了各级子阵阵元数的最优和次优分配表达式。仿真结果表明这些结论的正确性。 相似文献
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提出一种基于空时扩展虚拟传感器阵列的未知噪声环境下方位、俯仰、多普勒频移和相对时延四维参数联合估计新算法。未知噪声背景下的UN-MUSIC、UN-CLE等算法不易于完成多参数联合估计任务,而UN-ESPRIT算法又需要信号具有空、时域子空间旋转不变特性,对阵列结构要求严格。文中通过对原始数据的时延补偿等处理,利用虚拟数据阵的时移旋转不变特性,经由构建空时扩展波达方向矩阵同时获得诸参数的联合估计。虚拟传感器阵列的理论孔径为物理阵列的数倍,具有在低信噪比、未知分布噪声环境下更强的适应能力;且算法对于物理阵列阵元分布无特殊要求,具有很好的理论和实用价值。理论分析以及计算机仿真都证明了算法的有效性。 相似文献
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Space solar power shows great promise for future energy sources worldwide. Most central power stations operate with power capacity of 1000 MW or greater. Due to launch size limitations and specific power of current, rigid solar arrays, the largest solar arrays that have flown in space are around 50 kW. Thin-film arrays offer the promise of much higher specific power and deployment of array sizes up to several MW with current launch vehicles. An approach to early commercial applications for space solar power to distribute power to charge hand-held, mobile battery systems by wireless power transmission (WPT) from thin-film solar arrays in quasi-stationary orbits will be presented. Four key elements to this prototype will be discussed: (1) Space and near-space testing of prototype wireless power transmission by laser and microwave components including WPT space to space and WPT space to near-space HAA transmission demonstrations; (2) distributed power source for recharging hand-held batteries by wireless power transmission from MW space solar power systems; (3) use of quasi-geostationary satellites to generate electricity and distribute it to targeted areas; and (4) architecture and technology for ultra-lightweight thin-film solar arrays with specific energy exceeding 1 kW/kg. This approach would yield flight demonstration of space solar power and wireless power transmission of 1.2 MW. This prototype system will be described, and a roadmap will be presented that will lead to still higher power levels. 相似文献