The problems on passive fault-tolerant control of a spacecraft during its interorbital flight and the transition of a vehicle from the trajectory of its passive motion into a circular orbit at failures of the working jet engines are considered. The developed algorithms for reliable control of the spacecraft with stochastic stream of faults and obtained results are presented.
Stochastic Optimization of Fault-tolerant Spacecraft Control at Interorbital Flights
23.06.2021
2603169 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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