DocumentCode :
3492825
Title :
Attitude control of a CubeSat in a circular orbit using magnetic actuators
Author :
Oluwatosin, Ajayi Michael ; Hamam, Yskandar ; Djouani, Karim
Author_Institution :
Dept. of Electr. Eng., Tshwane Univ. of Technol., Tshwane, South Africa
fYear :
2013
fDate :
9-12 Sept. 2013
Firstpage :
1
Lastpage :
9
Abstract :
This paper deals with attitude tracking control of a spacecraft using magnetic actuators. The objective of this paper is to investigate the effectiveness of magnetic actuators for the Attitude Control System (ACS) of a CubeSat in a low earth circular orbit. This investigation is achieved via a proposed control law (set point regulator) based on the well known (model independent) PD controller. To validate this objective, two (2) cases representing the attitude manoeuvre were considered using SCILAB application software. A numerical orbit propagator was used to mimic the said circular orbit. Simulation results are presented showing the performance of the proposed solution.
Keywords :
PD control; artificial satellites; attitude control; control engineering computing; control system synthesis; magnetic actuators; ACS; CubeSat; SCILAB application software; attitude control system; attitude manoeuvre; attitude tracking control; circular orbit; control law; magnetic actuators; model independent PD controller; numerical orbit propagator; proportional-derivative controller; set point regulator; spacecraft; Angular velocity; Attitude control; Orbits; Quaternions; Satellites; Space vehicles; Torque;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
AFRICON, 2013
Conference_Location :
Pointe-Aux-Piments
ISSN :
2153-0025
Print_ISBN :
978-1-4673-5940-5
Type :
conf
DOI :
10.1109/AFRCON.2013.6757619
Filename :
6757619
Link To Document :
بازگشت