In-flight parametric identification and gyromoment stabilization of large-scale satellite

Actual problems on synthesis and analysis are considered for digital system of a gyromoment motion stabilization by a large-scale satellite with flexible weak damping structure. Elaborated methods for in-flight identification of the structure low resonance frequencies and a satellite inertia tensor, for construction of the gyromoment cluster turning laws, and also for synthesizing the algorithms of discrete filtering and digital control, are presented.