Title :
Magnetic attitude control using fuzzy logic
Author :
Heydari, Ali ; Pourtakdoust, Seid H. ; Heydari, Hamed
Author_Institution :
Dept. of Aerosp. Eng., Sharif Univ. of Technol., Tehran, Iran
Abstract :
A fuzzy controller has been suggested for attitude control of magnetic actuated satellites in order to calculate the desired mechanical torque based on the attitude error including error in the angles and their rates. The problem of selecting proper magnetic dipole based on the known desired mechanical torque has been investigated, two different methods for the purpose has been suggested and the performance of the attained fuzzy magnetic attitude controllers has been shown under two different simulated conditions.
Keywords :
artificial satellites; attitude control; electromagnetic actuators; fuzzy control; magnetic moments; attitude control; attitude error; fuzzy logic control; magnetic actuated satellite; magnetic dipole selection; mechanical torque; Attitude control; Coils; Equations; Fuzzy control; Fuzzy logic; Intelligent control; Neural networks; Satellites; Space technology; Torque control;
Conference_Titel :
Control Applications, (CCA) & Intelligent Control, (ISIC), 2009 IEEE
Conference_Location :
St. Petersburg
Print_ISBN :
978-1-4244-4601-8
Electronic_ISBN :
978-1-4244-4602-5
DOI :
10.1109/CCA.2009.5280979
