用于CATF多波束卫星表征的紧凑型低轮廓双线性ku波段馈源

Sasikanta Kumar, P. K. Mishra, S. K. Bandlamudi, Haindavi Manigilla, R. Renuka, S. Kumar, V. Hariharan
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引用次数: 1

摘要

在紧凑型天线试验设施(CATF)上,设计并成功实现了一种紧凑、低轮廓的ku波段馈源,用于多波束卫星有效载荷的表征。综合航天器(S/C)的应答器特性通常使用上行(U/L)和下行(D/L) CATF馈源安装在CATF的双馈板定位器上进行。通过为航天器定位器提供适当的方位角和仰角,在轨测试(IOT)位置与设施参考轴平行,用于有效载荷表征。该方法适用于单波束和足够宽波束覆盖的航天器。但是这种方法不能用于具有多个高增益波束的S/C,因为任何时候U/L或D/L波束都可以在CATF几何形状的焦点上,而其他波束将远离焦点。由于波束非常窄(波束宽度为0.8°3 dB),如果空间间隔高,可能无法使应答器饱和。为了满足这一关键要求,对CATF进行了几何分析,以找出每个光束在CATF焦平面上对应的馈电位置。本文在接下来的四节中详细讨论了满足CATF所有照明要求的紧凑型低轮廓Ku波段馈源的设计、方法和测量验证。该馈源用于综合多波束航天器GSAT 19、GSAT 11和GSAT 29的有效载荷表征。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Compact Low Profile Dual Linear Ku-band Feed for Multi-beam Satellite Characterization at CATF
A compact, low profile Ku-band feed is designed and realized successfully for characterization of multi-beam satellite payloads at Compact Antenna Test Facility (CATF). Transponder characterization of integrated spacecraft (S/C) is generally carried out using uplink (U/L) and downlink (D/L) CATF feeds mounted on twin feed plate positioner of CATF. By giving appropriate azimuth and elevation angle to spacecraft positioner, In Orbit Test (IOT) location is brought parallel to facility reference axis, for payload characterization. This method is suitable for spacecraft's with single and sufficiently broad beam coverage. But this same method cannot be used for S/C with multiple high gain beams, because any time either U/L or D/L beam can be in focus of CATF geometry and other beam will be away from the focus. As the beams are very narrow (0.8 deg 3 dB beam width) it may not be possible to saturate the transponder if the spatial separation is high. To meet this critical requirement, geometrical analysis of CATF is done to find out corresponding feed locations at CATF focal plane for each beam. In this paper in next four sections design aspects, methodology and measurement validation of compact low profile Ku band feeds, which meet all the illumination requirements of CATF are discussed in details. This developed feeds latter used for payload characterization of integrated multi-beam spacecraft GSAT 19, GSAT 11 and GSAT 29 in CATF.
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