Triaxial electrodynamic stabilization of a satellite via PID controller:

Alexander Yu. Aleksandrov; Sergey B. Ruzin

doi:10.21638/spbu10.2024.209

Authors

Alexander Yu. Aleksandrov St. Petersburg State University, 7–9, Universitetskaya nab., St. Petersburg, 199034, Russian Federation https://orcid.org/0000-0001-7186-7996
Sergey B. Ruzin St. Petersburg State University, 7–9, Universitetskaya nab., St. Petersburg, 199034, Russian Federation

DOI:

https://doi.org/10.21638/spbu10.2024.209

Abstract

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:

satellite, electrodynamic control, triaxial stabilization, Lyapunov — Krasovskii functional, PID controller

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References

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