Open AccessFeatures of Attitude Control of a Spacecraft, Equipped with Inertial Actuators
Author(s) -
М. В. Левский
Publication year - 2015
Publication title -
mehatronika, avtomatizaciâ, upravlenie
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.188
H-Index - 2
eISSN - 2619-1253
pISSN - 1684-6427
DOI - 10.17587/mau.16.188-195
Subject(s) - spacecraft , control moment gyroscope , angular acceleration , angular momentum , angular velocity , physics , rotation (mathematics) , acceleration , control theory (sociology) , position (finance) , inertial frame of reference , moment (physics) , rotation around a fixed axis , circular motion , attitude control , torque , angular displacement , classical mechanics , aerospace engineering , mathematics , computer science , engineering , control (management) , geometry , acoustics , astronomy , finance , artificial intelligence , economics , thermodynamics