Mathematical model of a flexible asymmetrical rotor for active magnetic bearing reaction wheel

Bibliographic Details
Parent link:MATEC Web of Conferences
Vol. 158 : Space Engineering.— 2018.— [01025, 5 p.]
Main Author: Polyakov M. Miroslav
Corporate Author: Национальный исследовательский Томский политехнический университет (ТПУ)
Other Authors: Lipovtsev A. Anatoliy, Lyanzburg V. Vladimir
Summary:Title screen
The paper introduces the mathematical model of rotor for active magnetic bearing reaction/momentum wheels, used as actuator in spacecraft attitude and orbit control system. Developed model is used for estimation of critical speeds and forced oscillation magnitudes with a glance of the rotor modes. Rotor is considered as a two-mass system, consisting of a shaft and a rim, active magnetic bearings are assumed to be a linear elastic springs. The equations of the rotor motion are derived using the Lagrange equation. Developed model is verified by comparing the calculated Campbell diagrams with the results of the finite-element modal analysis, performed in the ANSYS software.
Published: 2018
Subjects:
Online Access:https://doi.org/10.1051/matecconf/201815801025
http://earchive.tpu.ru/handle/11683/52910
Format: Electronic Book Chapter
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=659430