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.
Safwat, I., Elwakeel, A., Eliwa, A. E., & Abd Elsattar, A. (2010). Control of BLDC Motor for Satellite Momentum Exchange. The International Conference on Electrical Engineering, 7(7th International Conference on Electrical Engineering ICEENG 2010), 1-15. doi: 10.21608/iceeng.2010.33004
MLA
Ibrahim M. Safwat; Amgad S. Elwakeel; Abd Elfattah Eliwa; A. Abd Elsattar. "Control of BLDC Motor for Satellite Momentum Exchange". The International Conference on Electrical Engineering, 7, 7th International Conference on Electrical Engineering ICEENG 2010, 2010, 1-15. doi: 10.21608/iceeng.2010.33004
HARVARD
Safwat, I., Elwakeel, A., Eliwa, A. E., Abd Elsattar, A. (2010). 'Control of BLDC Motor for Satellite Momentum Exchange', The International Conference on Electrical Engineering, 7(7th International Conference on Electrical Engineering ICEENG 2010), pp. 1-15. doi: 10.21608/iceeng.2010.33004
VANCOUVER
Safwat, I., Elwakeel, A., Eliwa, A. E., Abd Elsattar, A. Control of BLDC Motor for Satellite Momentum Exchange. The International Conference on Electrical Engineering, 2010; 7(7th International Conference on Electrical Engineering ICEENG 2010): 1-15. doi: 10.21608/iceeng.2010.33004
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