Stabilization of Satellite Relative Equilibrium Using Magnetic and Lorentzian Moments
Author:
Publisher
Pleiades Publishing Ltd
Subject
Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering
Link
https://link.springer.com/content/pdf/10.1134/S0010952521050051.pdf
Reference50 articles.
1. Psiaki, M., Magnetic torque attitude control via asymptotic periodic linear quadratic regulation, J. Guid., Control, Dyn., 2001, vol. 24, no. 2, pp. 386–394.
2. Bushenkov, V.A., Ovchinnikov, M.Yu., and Smirnov, G.V., Attitude stabilization of a satellite by magnetic coils, Acta Astronaut., 2002, vol. 50, pp. 721–728. https://doi.org/10.1016/S0094-5765(02)00011-5
3. Lovera, M. and Astolfi, A., Spacecraft attitude control using magnetic actuators, Automatica, 2004, vol. 40, pp. 1405–1414.
4. Lovera, M. and Astolfi, A., Global magnetic attitude control of spacecraft in the presence of gravity gradient, IEEE Trans. On Aerospace and Electronic Systems, 2006, vol. 12, pp. 796–805.
5. Rehanoglu, M. and Hervas, J.R., Three-axis magnetic attitude control algorithm for small satellites, Proc. of the 5th Int. Conf. on Recent Advance Technologies, Istanbul, 2011, pp. 897–902.
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