Open AccessModelling the attitude dynamics of small spacecraft with a magnetic attitude control system in three-axis stabilization mode
Author(s) -
V. M. Kulkov,
V. M. Kulkov,
Yu. G. Egorov,
Ю Г Егоров,
S. O. Firsyuk,
С О Фирсюк,
V. V. Terentyev,
В. В. Терентьев,
A. O. Shemyakov,
A. O. Shemiakov
Publication year - 2019
Publication title -
doklady akademii nauk. rossijskaâ akademiâ nauk
Language(s) - English
Resource type - Journals
ISSN - 0869-5652
DOI - 10.31857/s0869-56524884377-382
Subject(s) - spacecraft , attitude control , control theory (sociology) , magnetic field , mode (computer interface) , physics , dynamics (music) , satellite , circular motion , angular velocity , control (management) , aerospace engineering , computer science , classical mechanics , engineering , acoustics , astronomy , quantum mechanics , artificial intelligence , operating system
The problem of modeling the attitude-control modes of small spacecraft with the use of electromagnetic systems, interacting with the Earths magnetic field is considered. A small spacecraft angular motion mathematical model is developed. A control law for magnetic attitude control system of small spacecraft is formulated. Results of satellite with magnetic attitude control system movement numerical modelling are presented.