Modelling the attitude dynamics of small spacecraft with a magnetic attitude control system in three-axis stabilization mode

Autor:	Yu. G. Egorov, V. V. Terentyev, S. O. Firsyuk, V. M. Kulkov, A. O. Shemyakov
Rok vydání:	2019
Předmět:	Physics Attitude control system Multidisciplinary Spacecraft business.industry Dynamics (mechanics) Mode (statistics) Magnetic field Circular motion Physics::Space Physics Satellite Astrophysics::Earth and Planetary Astrophysics Aerospace engineering business
Zdroj:	Доклады Академии наук. 488:377-382
ISSN:	0869-5652
Popis:	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.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::36ccc0f6d0b201e14f14f9e1b854ba75 https://doi.org/10.31857/s0869-56524884377-382 Zobrazit plný text záznamu