Authors :
O. B. Musa; C. T. Tofade; E. O. Oyewole; K. O. Orji-Daniels; O. E. Haruna
Volume/Issue :
Volume 11 - 2026, Issue 8 - August
Google Scholar :
https://tinyurl.com/y434mmuh
DOI :
https://doi.org/10.38124/ijisrt/26aug1575
Note : A published paper may take 4-5
working days from the publication date to appear in PlumX Metrics, Semantic Scholar, and
ResearchGate.
Abstract :
Reaction wheels are widely used as momentum-exchange actuators for spacecraft attitude control; however,
conventional mechanical bearings introduce friction, wear, imbalance forces, and microvibrations that can affect pointing
accuracy. Active magnetic bearings (AMBs) provide a contactless alternative by actively regulating electromagnetic forces
to maintain rotor position. This paper presents the design and implementation of an AMB control system for a laboratoryscale reaction wheel using electromagnetic actuators, non-contact displacement sensors, current-controlled power amplifiers,
a digital controller, and proportional-integral-derivative (PID) control.
Keywords :
Active Magnetic Bearing, Reaction Wheel, Spacecraft Attitude Control, Magnetic Levitation, Rotor Dynamics, PID Control, Microvibration, Electromagnetic Actuator.
References :
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Reaction wheels are widely used as momentum-exchange actuators for spacecraft attitude control; however,
conventional mechanical bearings introduce friction, wear, imbalance forces, and microvibrations that can affect pointing
accuracy. Active magnetic bearings (AMBs) provide a contactless alternative by actively regulating electromagnetic forces
to maintain rotor position. This paper presents the design and implementation of an AMB control system for a laboratoryscale reaction wheel using electromagnetic actuators, non-contact displacement sensors, current-controlled power amplifiers,
a digital controller, and proportional-integral-derivative (PID) control.
Keywords :
Active Magnetic Bearing, Reaction Wheel, Spacecraft Attitude Control, Magnetic Levitation, Rotor Dynamics, PID Control, Microvibration, Electromagnetic Actuator.