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ADDITIONAL LAUNCHING AND APPROACH OF A SPACE ROBOT FOR SERVICING A GEOSTATIONARY SATELLITE
ДОПОЛНИТЕЛЬНОЕ ВЫВЕДЕНИЕ И СБЛИЖЕНИЕ КОСМИЧЕСКОГО РОБОТА ДЛЯ ОБСЛУЖИВАНИЯ ГЕОСТАЦИОНАРНОГО СПУТНИКА
2021
Izvestiia Samarskogo nauchnogo tsentra Rossiiskoi akademii nauk
ДОПОЛНИТЕЛЬНОЕ ВЫВЕДЕНИЕ И СБЛИЖЕНИЕ КОСМИЧЕСКОГО РОБОТА ДЛЯ ОБСЛУЖИВАНИЯ ГЕОСТАЦИОНАРНОГО СПУТНИКА
Preserved Fulltext
The problems of additional launching a space robot into a geostationary orbit and approaching a geostationary satellite for its maintenance are considered. The robot's attitude and orbit control system uses an electric propulsion unit, a propulsion system based on eight electric thermo-catalytic engines with pulse-width modulation of their thrust, and a gyro moment cluster based on four single-gimbal control moment gyroscopes (gyrodines). Numerical results are presented that demonstrate the
doi:10.37313/1990-5378-2021-23-2-75-83
fatcat:lx277ccknna6jm2tiama4ey7uu