In the article the methods for calculation of dynamic object automatic control system efficiency with active fault tolerance property is offered. Results of estimation and comparative analysis for system efficiency of classic attitude control system for small satellite and control system with fault tolerance automatic control object in out-of-staff mode with faults in system element are presented .
satellite, orientation, stabilization, automatic control object, active fault tolerance, efficiency
"Raschet эffektyvnosty prymenenyia otkazoustoichyvoi systemы upravlenyia oryentatsyei y stabylyzatsyy sputnyka" ,
Information Processing Systems,