敏捷陆地测量卫星的姿态制导、导航和鲁棒控制

2017 8th International Conference on Recent Advances in Space Technologies (RAST) Pub Date : 2017-06-01 DOI:10.1109/RAST.2017.8003017

Y. Somov, S. Butyrin, S. Somov

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引用次数: 2

摘要

研究了用于地球表面测量的敏捷航天器的姿态制导、导航和鲁棒陀螺仪力矩控制问题。本文提出了航天器姿态控制系统在主要模态下的动态研究方法，并利用少过量陀螺仪方案对陀螺力矩簇进行了数字控制。

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Attitude guidance, navigation and robust control of an agile land-survey satellite

We consider problems on attitude guidance, navigation and robust gyromoment control of the agile spacecraft for surveying the Earth surface. We present developed methods for dynamic research of the spacecraft attitude control system at the main modes under disturbances and digital control of the gyro moment clusters by the few-excessive gyrodine schemes.

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2017 8th International Conference on Recent Advances in Space Technologies (RAST)

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