Geodesic
Triaxial electrodynamic stabilization of a satellite via PID controller
Vestnik Sankt-Peterburgskogo universiteta. Prikladnaâ matematika, informatika, processy upravleniâ, Tome 20 (2024) no. 2, pp. 244-254 Cet article a éte moissonné depuis la source Math-Net.Ru

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A satellite moving on a circular equatorial orbit is considered. The satellite is equipped with a controlled magnetic moment and a controlled electrostatic charge. The problem of triaxial stabilization in the orbital frame is studied. The electrodynamic control system is proposed. In addition, to improve characteristics of transient processes, PID controller of a special form is used. With the aid of the Lyapunov direct method, asymptotic stability conditions of the program mode are obtained. The results of computer simulation are provided demonstrating the efficiency of the developed approach.
Keywords: electrodynamic control, triaxial stabilization, Lyapunov — Krasovskii functional, PID controller.
Mots-clés : satellite 
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A. Yu. Aleksandrov; S. B. Ruzin. Triaxial electrodynamic stabilization of a satellite via PID controller. Vestnik Sankt-Peterburgskogo universiteta. Prikladnaâ matematika, informatika, processy upravleniâ, Tome 20 (2024) no. 2, pp. 244-254. http://geodesic.mathdoc.fr/item/VSPUI_2024_20_2_a8/

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