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Rotation matrix-based finite-time attitude synchronization control for flexible spacecrafts with unknown inertial parameters and actuator faults

Flexible SpacecraftsNonlinear ControlEngineeringAerospace EngineeringRobust ControlMechanical SystemsUnknown Inertial ParametersSystems EngineeringSpacecraft Attitude ControlFault-tolerant ControlActuator FaultsTracking ControlStability