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