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A NOVEL APPROACH TO MICROWAVE INTERFEROMETRIC RADIOMETRY IN THE GEOSTATIONARY ORBIT USING FORMATION FLIGHT

机译:使用形成飞行地球静止轨道微波干涉辐射测量的新方法

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A novel technique for Earth-observation microwave interferometric radiometry using satellite formation flight is presented. The concept allows large apertures of unprecedented sizes to be synthesised by means of antennas mounted on several free-flying platforms performing interferometry. The size of the synthesised aperture is determined by the furthest distance between the free-flying satellites. The concept is applicable to wide range of microwave frequencies, meaning that the large aperture may be applied to achieve unprecedented spatial resolution, to extend Earth observation radiometry to unprecedented long wavelengths, or to enable radiometry in the geostationary orbit. Two such concepts are presented, and as an example they are applied to geostationary radiometry at 10 GHz. The first concept employs a rotating Y-shaped interferometric radiometer in formation with a constellation of nine free-flying microsatellites. The effective diameter of the synthesised aperture is 14.4m, which produces a spatial resolution of 79.5 km at 10 GHz from the geostationary orbit. The total mass of the constellation can be within 2 tonnes, which may be deployed on a single launch vehicle. The second concept is a constellation of six formation-flying radiometers, which produce apertures of 28.8m, and produces a spatial resolution of 39.8 km at 10 GHz. While this configuration is capable of producing larger effective apertures, the total mass can exceed 5 tonnes, and may require multiple launches and rendezvous at the operational orbit. Both of these concepts can be scaled up for larger apertures, and are bound primarily by the number of satellites deployable in the constellation. The free-flying nature of the concept means they are susceptible to interferometric performance degradation by array deformation. The effect of deviation on the radiometric resolution is explored and found, concluding that deviation as small as 0.1A can lead to performance degradation of up to 20 K. Annual Al' required to maintain such constellations are also found at up to 2.23 m/s annually.
机译:介绍了使用卫星形成飞行的地球观察微波干涉辐射测定的新技术。该概念允许通过安装在执行干涉测量的几种自由飞行平台上的天线合成未夹持的尺寸的大孔。合成孔径的尺寸由自由飞行卫星之间的最远距离决定。该概念适用于广泛的微波频率,这意味着可以应用大孔径以实现前所未有的空间分辨率,以将地球观察辐射率延伸到前所未有的长波长,或者能够在地球静止轨道中启用辐射测量。提出了两个这样的概念,并且作为一个示例,它们在10GHz下应用于地静止辐射测量。第一个概念采用旋转Y形干涉辐射计,形成九个自由飞卫星的星座。合成孔径的有效直径为14.4M,从地球静止轨道产生10 GHz的空间分辨率为79.5km。星座的总质量可以在2吨内,这可以部署在一个发射车辆上。第二个概念是六个形成 - 飞辐射仪的星座,其产生28.8米的孔,并在10GHz下产生39.8km的空间分辨率。虽然这种配置能够产生较大的有效孔,但总质量可以超过5吨,并且可能需要在操作轨道上进行多次发射和结合。这两个概念都可以缩放较大的孔径,并且主要由星座中部署的卫星数量绑定。概念的自由飞行意味着它们易于通过阵列变形的干涉性能下降。探讨偏离辐射分辨率的效果并发现,得出结论,小于0.1A的偏差可能导致高达20K的性能下降,每年的AL'需要维持此类星座,也有高达2.23米/秒。每年。

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