
Attitude Control of Spacecraft by Two Variable-Speed Control Moment Gyros
Author(s) -
Jaehyun Jin
Publication year - 2015
Publication title -
je-eo lobos siseutem haghoe nonmunji/jeeo robot siseutem hakoe nonmunji
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.215
H-Index - 11
eISSN - 2233-4335
pISSN - 1976-5622
DOI - 10.5302/j.icros.2015.15.0166
Subject(s) - control moment gyroscope , torque , control theory (sociology) , attitude control , spacecraft , moment (physics) , reaction wheel , actuator , gyroscope , angular velocity , direct torque control , quaternion , control (management) , engineering , computer science , physics , control engineering , aerospace engineering , mathematics , classical mechanics , geometry , induction motor , electrical engineering , artificial intelligence , voltage , thermodynamics