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ADDITIONAL LAUNCHING AND APPROACH OF A SPACE ROBOT FOR SERVICING A GEOSTATIONARY SATELLITE
Author(s) -
Yevgeny Somov,
Sergey Butyrin,
Sergey Somov
Publication year - 2021
Publication title -
izvestiâ samarskogo naučnogo centra rossijskoj akademii nauk
Language(s) - English
Resource type - Journals
ISSN - 1990-5378
DOI - 10.37313/1990-5378-2021-23-2-75-83
Subject(s) - geostationary orbit , gimbal , satellite , gyroscope , aerospace engineering , computer science , propulsion , moment (physics) , thrust , payload (computing) , cubesat , attitude control , simulation , engineering , physics , network packet , computer network , classical mechanics
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 effectiveness of the developed discrete guidance and control algorithms.

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