DocumentCode :
1936536
Title :
A high precision attitude determination and control system for the UYS-1 nanosatellite
Author :
Chaurais, J.R. ; Ferreira, H.C. ; Ishihara, J.Y. ; Borges, R.A. ; Kulabukhov, A.M. ; Larin, V.A. ; Belikov, V.V.
Author_Institution :
Electr. Eng. Dept., Univ. of Brasilia, Brasilia, Brazil
fYear :
2013
fDate :
2-9 March 2013
Firstpage :
1
Lastpage :
12
Abstract :
This paper presents the design of a high precision attitude determination and control system for the UYS-1 Ukrainian nanosatellite. Its main task is the 3-axis stabilization with less than 0.5° angle errors, so the satellite may take high precision photos of Earth´s surface. To accomplish this task, this system comprises a star tracker and three reaction wheels. To avoid external disturbances and actuators faults, a PD-type and a PID-type robust controllers are simulated and the results are compared to an empirically adjusted PD controller.
Keywords :
actuators; aerospace control; artificial satellites; attitude control; robust control; three-term control; 3-axis stabilization; Earth surface; PID-type controllers; UYS-1 nanosatellite; actuators faults; control system; high precision attitude determination; high precision photos; satellite; star tracker; Angular velocity; Attitude control; Earth; Position measurement; Satellites; Torque; Wheels; Attitude Determination and Control System; PD; PID; Robust H Controller;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2013 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4673-1812-9
Type :
conf
DOI :
10.1109/AERO.2013.6496981
Filename :
6496981
Link To Document :
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