A Time-Periodic Control Law for Satellite Magnetic Stabilization - Volume 7 Number 3 (Jun. 2017) - ijmo
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General Information
Editor-in-chief
Prof. Adrian Olaru
University Politehnica of Bucharest, Romania
I'm happy to take on the position of editor in chief of IJMO. It's a journal that shows promise of becoming a recognized journal in the area of modelling and optimization. I'll work together with the editors to help it progress.
IJMO 2017 Vol.7(3): 168-172 ISSN: 2010-3697
DOI: 10.7763/IJMO.2017.V7.578

A Time-Periodic Control Law for Satellite Magnetic Stabilization

Adrian-Mihail Stoica and Vasile Dragan
Abstract—The paper presents a design methodology for the automatic control system of a satellite with magnetic actuators taking into account the time periodic variation of the Earth’s magnetic field. The design method is based on using an optimal 2 H controller with periodic coefficients. These coefficients depend on the solution of a specific system of coupled Riccati type equations. An iterative numerical algorithm to solve such system is also presented. The proposed design procedure is illustrated by a case study for a CubSat in which the benefits of using a a time-periodic controller are emphasized.

Index Terms—H optimal control, satellite stabilization, system of coupled Riccati equations, time periodic control law.

A.-M. Stoica is with the University “Politehnica” of Bucharest, Faculty of Aerospace Engineering, Str. Polizu, No. 1, Ro-011061, Bucharest, Romania (e-mail: adrian.stoica@upb.ro).
V. Dragan is with the Institute of Mathematics “Simion Stoilow” of the Romanian Academy, Bucharest, Romania (e-mail: vasile.dragan@imar.ro).

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Cite: Adrian-Mihail Stoica and Vasile Dragan, "A Time-Periodic Control Law for Satellite Magnetic Stabilization," International Journal of Modeling and Optimization vol. 7, no. 3, pp. 168-172, 2017.

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