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Diagnosis and Reconfiguration of the Spacecraft Fault Tolerant Gyromoment Control Systems

Yevgeny Somov, Valentin Makarov, Vladimir Matrosov
Methods for modelling and detection of the causes of anomalous functioning the automatic control systems and practical methods for analysis of the anomalous situations, are presented. Methods for consecutive classification of onboard equipment failures and control loop reconfiguration are considered. Some results on analysis of the gyromoment attitude control systems for the Earth sensing spacecraft, are represented.
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