Title
L1 Adaptive Attitude Control For A Picoscale Satellite Test Bed
Abstract
Smaller and more agile space assets, such as picoscale satellites, have become one of the promising focuses for space missions because of the benefits in cost reduction, enhanced flexibility, survivability, and reliability. A simple magnetic torque coil-based attitude control system is proposed here for a one unit picoscale satellite test bed using an L1 adaptive controller. A pointing accuracy of 2 deg is achieved in both a one-axis ground test bed and three-axis control simulation.
Publication Date
4-1-2015
Publication Title
IEEE Transactions on Aerospace and Electronic Systems
Volume
51
Issue
2
Number of Pages
1147-1154
Document Type
Article
Personal Identifier
scopus
DOI Link
https://doi.org/10.1109/TAES.2014.120175
Copyright Status
Unknown
Socpus ID
84934284470 (Scopus)
Source API URL
https://api.elsevier.com/content/abstract/scopus_id/84934284470
STARS Citation
Sease, Bradley; Yang, Qinmin; Xu, Yunjun; Che, Jiaxing; and Cao, Chengyu, "L1 Adaptive Attitude Control For A Picoscale Satellite Test Bed" (2015). Scopus Export 2015-2019. 239.
https://stars.library.ucf.edu/scopus2015/239