This paper presents an approach to an Advanced Fast Disturbance Rejection Proportional-Integral (AFDR-PI) control system based on a benchmark plant model description. The controller is designed for a balance between performance (response time) and robustness (stability margins). The proposed algorithm associated with the mathematical model has been carried out under MATLAB/SIMULINK environment. A comparison between the Proportional-Integral (PI) controller and AFDR-PI controller has been introduced with applied step input disturbance to the input of the control system. The conclusion is that the AFDR-PI controller has the same tracking performance (time response requirements) as the PI controller, and succeeds to reject the disturbance signal higher than the PI controller (robustness requirements).
Gamal, B. E., Ouda, A., El-Halwagy, Y., & El-Nashar, G. (2015). Advanced Fast Disturbance Rejection PI Controller for DC Motor Position Control. International Conference on Aerospace Sciences and Aviation Technology, 16(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 – May 26 - 28, 2015), 1-12. doi: 10.21608/asat.2015.22942
MLA
Bahaa El-den Gamal; A. N. Ouda; Y. Z. El-Halwagy; G. A. El-Nashar. "Advanced Fast Disturbance Rejection PI Controller for DC Motor Position Control". International Conference on Aerospace Sciences and Aviation Technology, 16, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 – May 26 - 28, 2015, 2015, 1-12. doi: 10.21608/asat.2015.22942
HARVARD
Gamal, B. E., Ouda, A., El-Halwagy, Y., El-Nashar, G. (2015). 'Advanced Fast Disturbance Rejection PI Controller for DC Motor Position Control', International Conference on Aerospace Sciences and Aviation Technology, 16(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 – May 26 - 28, 2015), pp. 1-12. doi: 10.21608/asat.2015.22942
VANCOUVER
Gamal, B. E., Ouda, A., El-Halwagy, Y., El-Nashar, G. Advanced Fast Disturbance Rejection PI Controller for DC Motor Position Control. International Conference on Aerospace Sciences and Aviation Technology, 2015; 16(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 – May 26 - 28, 2015): 1-12. doi: 10.21608/asat.2015.22942
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