Title
Optimal Attitude Control Allocation Via The B-Spline Augmented Virtual Motion Camouflage Method
Abstract
Instantaneous three-axis attitude control in many picoscale satellites is achieved by combining magnetic torque coils with other control devices such as thrusters. A B-spline augmented virtual motion camouflage method is presented to maximize the usage of magnetic torque coils and minimize that of thrusters, while calculating attitude guidance commands.
Publication Date
7-1-2015
Publication Title
IEEE Transactions on Aerospace and Electronic Systems
Volume
51
Issue
3
Number of Pages
1774-1780
Document Type
Article
Personal Identifier
scopus
DOI Link
https://doi.org/10.1109/TAES.2014.110748
Copyright Status
Unknown
Socpus ID
84942887356 (Scopus)
Source API URL
https://api.elsevier.com/content/abstract/scopus_id/84942887356
STARS Citation
Develle, Mike and Xu, Yunjun, "Optimal Attitude Control Allocation Via The B-Spline Augmented Virtual Motion Camouflage Method" (2015). Scopus Export 2015-2019. 447.
https://stars.library.ucf.edu/scopus2015/447