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Estimation of the Minimal Duration of an Attitude Change for an Autonomous Agile Earth-Observing Satellite

机译:估计自主敏捷地球观察卫星的态度变化的最小持续时间

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Most of the currently active Earth-observing satellites are entirely controlled from the ground: observation plans are regularly computed on the ground (typically each day for the next day), uploaded to the satellite using visibility windows, and then executed onboard as they stand. Because the possible presence of clouds is the main obstacle to optical observation, meteorological forecasts are taken into account when building these observation plans. However, this does not prevent most of the performed observations to be fruitless because of the unforeseen presence of clouds. To fix this problem, the possibility of equipping Earth-observing satellites with an extra instrument dedicated to the detection of the clouds in front of it, just before observation, is currently considered. But, in such conditions, decision upon the observations to be performed can be no longer made offline on the ground. It must be performed online onboard, because it must be performed at the last minute when detection information is available and because visibility windows between Earth-observing satellites and their control centers are short and rare. With agile Earth-observing satellites which are the next generation ones, decision-making upon observation requires the computing of an as short as possible attitude trajectory allowing the satellite to point to the right ground area within its visibility window. In this paper, we show the results of an experiment consisting in using a continuous constraint satisfaction problem solver (RealPaver) to compute such optimal trajectories online onboard.
机译:大多数目前活跃的地球观测卫星完全由地面控制:观察计划在地面上经常计算(通常是第二天每天),使用可见性窗口上传到卫星,然后在它们站立时执行。由于云的可能存在是光学观察的主要障碍,因此在构建这些观察计划时考虑了气象预测。然而,由于未经预见的云存在,这并不能阻止大多数所表的观察结果。为了解决这个问题,目前考虑在观察之前,用额外的仪器用额外的仪器向地球观测卫星进行额外的仪器的可能性。但是,在这种情况下,在待执行的观察结果中可以不再离线在地面上进行决定。它必须在线执行船上执行,因为当检测信息可用时必须在最后一分钟执行,因为地球观测卫星和控制中心之间的可见性窗口是短而罕见的。对于作为下一代的敏捷地球观察卫星,观察的决策需要计算尽可能短的姿态轨迹,允许卫星指向其可见性窗口内的右接地区域。在本文中,我们展示了在使用连续约束满意问题求解器(RealPaver)的实验结果,以计算板载在线的这种最佳轨迹。

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