Control of BLDC Motor for Satellite Momentum Exchange | ||||
The International Conference on Electrical Engineering | ||||
Article 46, Volume 7, 7th International Conference on Electrical Engineering ICEENG 2010, May 2010, Page 1-15 PDF (1.28 MB) | ||||
Document Type: Original Article | ||||
DOI: 10.21608/iceeng.2010.33004 | ||||
View on SCiNiTO | ||||
Authors | ||||
Ibrahim M. Safwat1; Amgad S. Elwakeel1; Abd Elfattah Eliwa1; A. Abd Elsattar2 | ||||
1Egyptian Armed Force. | ||||
2Prof. Dr., Ain Shams University. | ||||
Abstract | ||||
Abstract: The reaction wheel is a small fraction of the spacecraft total mass. It permits very precise changes in spacecraft attitude. A novel model of a single-axis position control on a satellite is designed using Brushless DC (BLDC) motor with a resolver to exchange the momentum of the satellite as a reaction wheel. The technique of attitude control is based on considering the moment of inertia of the satellite as a part of the moment of inertia of BLDC motor, so the control on a satellite becomes the control of a Brushless DC motor. Two kinds of controllers are used (PID) controller and (FLC). The performance of both controllers is evaluated to explain the main characteristics of each one. | ||||
Keywords | ||||
Attitude control of satellite; Mathematical model of Brushless DC Motor (BLDC); Proportional Integrator Differentiative (PID) controller; Fuzzy logic controller (FLC) | ||||
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