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Preshaping Profiler for Flexible Spacecraft Rest-to-Rest Maneuvers

机译:Preshaping Profiler,适用于灵活的航天器休息休息的操作

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A new feedforward algorithm for flexible spacecraft maneuvers is presented. We call this preshaping profiler the nil-mode-exciting (NME) profiler. This algorithm is designed particularly for single-axis rest-to-rest rotational maneuvers (switching maneuvers) with linear actuators. Generally spacecraft with large flexible structure has a lot of large-mass flexible-modes. Therefore, uncertainity of high-order modes needs to be considered for high-accuracy controller design. This paper presents an extra-insensitive maneuvering method which overcomes above-mentioned difficulties. This algorithm includes a preshaping profiler formulated from sampling function (also known as sinc function), consequently feedforward control inputs generated from the preshaping profiler have no frequency response above a certain designed frequency. Therefore residual vibration at the end-point of maneuver can be highly reduced with minimum loss of maneuver agility.
机译:提出了一种新的柔性航天器机动的前馈算法。我们称之为Preshaping Profiler Nil-Mode-Eigining(NME)分析器。该算法特别设计用于单轴休息旋转机动(开关机动),具有线性致动器。通常具有大柔性结构的航天器具有大量大量柔性模式。因此,需要考虑高级模式的优化模式的不确定性。本文介绍了一种超敏感的操纵方法,克服了上述困难。该算法包括由采样函数(也称为SINC功能)配制的预先开采分析器,因此从预热分析器产生的前馈控制输入没有高于特定设计频率的频率响应。因此,由于机动敏捷性最小损耗,机动终点的剩余振动可以高度降低。

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