Ensuring the Survivability of Spacecraft Control System at Critical Failures in Flywheel Cluster

Y. Somov, S. Butyrin, S. Somov
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Abstract

A method for ensuring the survivability of a spacecraft attitude control system with minimally redundant cluster of the flywheels and magnetic actuator at the faults of any flywheels are presented. The results of computer simulation were obtained and it was found if any two of the four flywheels according to the General Electric scheme fail, digital control of the flywheel cluster and magnetic drive allows the Earth-observing satellite to maintain observation of given terrestrial targets.
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飞轮群关键故障下航天器控制系统的生存保障
提出了一种在任意飞轮出现故障时,保证航天器姿态控制系统最小冗余度飞轮和磁致动器簇的生存能力的方法。计算机仿真结果表明,如果通用电气方案的四个飞轮中的任何两个发生故障,对飞轮群和磁驱动的数字控制可以使地球观测卫星保持对给定地面目标的观测。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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