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

Socpus ID

84942887356 (Scopus)

Source API URL

https://api.elsevier.com/content/abstract/scopus_id/84942887356

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