Fault Tolerant Gyromoment Control of Information Spacecraft with Fine Pointing of Large-scale Antennas∗

Methods for modeling and detection of anomalous functioning the automatic control systems and practical methods for active analysis of the anomalous situations, are presented. Methods for consecutive classification of onboard equipment failures and control loop reconfiguration are considered. We present some results on fault-tolerant attitude gyromoment control of an information satellite with precise pointing of the large-scale flexible antennas.