作者: Renuganth Varatharajoo
DOI: 10.1016/J.ACTAASTRO.2003.12.004
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摘要: Abstract The idea of combining the satellite attitude control system and electrical power is investigated in this article. combined energy (CEACS) concept based on a double counter rotating flywheel assembly serving simultaneously for storage tasks. In past years, synergistic was proposed larger spacecraft, but until today comprehensive end-to-end demonstration small satellites still has not been performed. On basis, investigation narrowed to consideration at inception study. First, CEACS architecture presented along with its mathematical models. Then, numerical treatments sufficient magnitude are performed, which allow an assessment system's merits. simulation results pertaining ideal non-ideal test cases indicate that judiciously attractive future satellites.