Nonlinear Dynamics of Fault Tolerant Spacecraft Control Systems

摘要

We present new results on creation and employment of nonlinear methods and algorithms for research of logic-dynamic fault-tolerant control systems and applications these results to precision gyromoment attitude control systems on informationsatellites (for remote sensing, communication, navigation and geodetic) developed by the leading Russian State Research and Production Associations: Central Specialized Design Bureau (TsSKB), Samara, Applied Mechanics (NPO PM), Krasnoyarsk.