2007
DOI: 10.1109/tgrs.2007.898093
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Analysis of Array Distortion in a Microwave Interferometric Radiometer: Application to the GeoSTAR Project

Abstract: Abstract-The Geostationary Synthetic Thinned Array Radiometer represents a promising new approach to microwave atmospheric sounding from geostationary orbit based on passive interferometry. Distortion due to mechanical or thermal constraints produces a displacement of the ideal antenna positions in the array that causes sampling errors. In this paper, the impact of array distortion on radiometric error is analyzed in detail so as to identify the dominant sources of error. A preliminary analysis showing that ar… Show more

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Cited by 25 publications
(11 citation statements)
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References 13 publications
(31 reference statements)
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“…The degree to which the error propagates in this method, however, is also sensitive to the distribution of the beacons. Furthermore, the recovered ∆z and ∆φ are strongly coupled, as also demonstrated in [29]. To account for this coupling, the expression (18) is generalised using covariance matrices.…”
Section: B Receiver Phase and Baseline Calibration Using Airborne Bementioning
confidence: 89%
“…The degree to which the error propagates in this method, however, is also sensitive to the distribution of the beacons. Furthermore, the recovered ∆z and ∆φ are strongly coupled, as also demonstrated in [29]. To account for this coupling, the expression (18) is generalised using covariance matrices.…”
Section: B Receiver Phase and Baseline Calibration Using Airborne Bementioning
confidence: 89%
“…The visibility samples are then taken by interpolating the sampling pattern ( Fig. 8) within this map, and the effect of outof-plane deviation w is approximated as constant phase errors in the individual antennas as performed in [20]. The individual antenna voltage pattern F n and beamwidth are modeled after the horn antennas applied on the GeoSTAR demonstrator [16] linearly scaled to our 3λ separation such that = 0.211 sr. Circular symmetry is assumed for the beam about its boresight with no pointing errors and all antennas are identical.…”
Section: Simulating Array Performancementioning
confidence: 99%
“…(1) 结构变形与误差对电性能的影响。关于星 载天线阵面误差方面,WANG [65] 分析了天线典型机 械误差和随机误差对天线电性能影响,并指出星载 有源相控阵天线为了获得-10 dBi 平均副瓣电平, 阵 面误差须控制在 1%波长范围以内。OSSOWSKA 等 [66] 指出星载可展开有源相控阵天线阵面变形主 要有三种--对称变形、 非对称变形和随机变形(图 11),并分析了三种变形对天线电性能的影响。 ZULCH 等 [67] 针对美国空军和 NASA 机构研制的低 轨道 L 波段 1.25 GHz 的星载有源相控阵天线, 分析 了天线阵面变形对天线增益和对 GMTI 的影响。 (2) 电磁电路校准与补偿。TORRES 等 [68] 分析 了振动和热变形对天线电性能的影响,并通过外部 相位参考方法来校正阵元位置误差。PIERRO 等 [69] 分析了最大变形量为 10 cm 的阵面变形对中轨道星 载可展开有源相控阵天线波形和 GMTI 的影响。针 对结构变形补偿和校准技术,TAKAHASHI 等 [70] 对 星载可展开有源相控阵天线发射升空时振动和在轨 热振动导致的结构变形提出了一种补偿方法,即分 三个阶段校准:初始校准、发射前校准和在轨校准, 最后对每个阵元的相位误差进行补偿。LIER 等 [71] 针对星载 Ku 频段(17.3~17.8 GHz)有源相控阵天线 阵面变形,提出了控制电路编码校准技术。 (3) 形状记忆与自动补偿。SONG 等 [72] 将一种 形状记忆合金丝嵌入蜂窝结构体中,用于精密空间 结构的热变形补偿。 MCWATTERS 等 [73] 针对星载可 展开有源相控阵天线在轨热环境、 自身产生的热量、 卫星平台的振动和机械变形,提出了天线自动校准 和计量系统的概念,用于纠正在轨过程中的相位误 差和机械变形。PETERMAN 等 [74] [86] ,这是因为它具有如下特点:RF MEMS 不 仅可以大幅缩小相控阵天线体积,还可减轻重量; 由于 MEMS T/R 组件在低功耗方面表现突出,能减 轻相控阵扫描阵列的散热问题,延长其寿命;相比 于传统 T/R 组件,MEMS T/R 组件的插入损耗低, 故仅需要一般相控阵中 25%~50%的 T/R 组件数量 即可满足天线系统功能需要 [87] ;由于 MEMS 器件 的高线性度、宽带性能和开关高隔离度的特点,应 用 MEMS T/R 组件还能提高相控阵天线带宽、灵敏 度以及降低瞄准误差。 [51] (图 22)、单轴卷开 式展开结构(图 23)和双线轴展开结构(图 24) [90] 等三 种展开机构形式。复杂的展开机构是确保天线系统 能否正常工作的首选条件,因此应绝对保证展开机 构的可靠性。 …”
Section: 国外研究现状 国外主要从三个方面来研究星载阵列天线的 结构设计。unclassified