DocumentCode :
3670220
Title :
Low cost attitude estimation system. Performance evaluation on an airbearing based testbed
Author :
F. von Bergen;J. Giribet;P. Martos
Author_Institution :
GPSIC - Dept. of Electrical Engineering, University of Buenos Aires, Buenos Aires, Argentina
fYear :
2015
Firstpage :
25
Lastpage :
30
Abstract :
In this work, a low-cost attitude navigation system for spacecrafts is presented. The system fuses measurements from a three axis MEMS gyroscope and a CCD camera that identifies a known pattern of points (which emulate the stars). The system has been implemented on an ARM Cortex-A8 processor, running a GNU/Linux operating system. The developed attitude system was tested on an air-bearing testbed as experimental validation.
Keywords :
"Estimation","Quaternions","Sensors","Cameras","Gyroscopes","Navigation","Angular velocity"
Publisher :
ieee
Conference_Titel :
Embedded Systems (CASE), 2015 Sixth Argentine Conference on
Print_ISBN :
978-9-8745-5234-1
Type :
conf
DOI :
10.1109/SASE-CASE.2015.7295843
Filename :
7295843
Link To Document :
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