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.
Optimal attitude control allocation via the B-spline augmented virtual motion camouflage method
IEEE Transactions on Aerospace and Electronic Systems ; 51 , 3 ; 1774-1780
01.07.2015
764696 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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