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Launching 2009: The NigeriaSat-2 mission – High-performance Earth observation with a small satellite

机译:2009年发射:NigeriaSat-2任务–用小型卫星进行高性能地球观测

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The NigeriaSat-2 mission is a high-resolution imaging mission currently under construction and due for launch in2009. This paper will emphasise the potential of a mission of this type, particularly highlighting missionperformance parameters such as image throughput and ground coverage rate. It will also underscore the versatilityof the platform by highlighting the extensive modes of operation that are possible, and the possibilities that thesecould have for the end customer.It will then discuss the technological advances that allow operational high resolution imagery to be captured onboard a 300kg satellite. Attention will be paid to the mechanical engineering challenges of isolating the payloadfrom thermal distortions introduced into the rest of the spacecraft platform and hence the novel way in which SSTLhas solved this, allowing a very high geolocation accuracy to be achieved.Finally included in the paper will be a discussion on the advanced attitude and orbit control sub-system, whichprovides both high stability during imaging as well as high agility and a fast slew capability to transition betweenimaging opportunities.
机译:NigeriaSat-2任务是一项高分辨率成像任务,目前正在建设中,计划于2000年发射 2009年。本文将重点介绍此类任务的潜力,特别是突出任务 性能参数,例如图像吞吐量和地面覆盖率。它还将强调多功能性 通过强调可能的广泛操作模式以及这些可能性 可能会给最终客户。 然后,它将讨论允许在高分辨率图像上捕获可操作的高分辨率图像的技术进步。 登上300公斤重的卫星。将关注隔离有效载荷的机械工程挑战 来自引入航天器平台其余部分的热变形,以及由此产生的SSTL新颖方法 解决了这个问题,可以实现很高的地理位置精度。 最后,本文将讨论高级姿态和轨道控制子系统,该子系统 提供成像期间的高稳定性以及高敏捷性和快速转换能力,可在 影像机会。

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