Extensive Numerical Simulation of a Magnetically Actuated Satellite’s Rotation around the Direction toward the Sun with Data from the Solar Sensors Only
Author:
Publisher
Pleiades Publishing Ltd
Subject
Computational Mathematics,Modeling and Simulation
Link
https://link.springer.com/content/pdf/10.1134/S2070048223050083.pdf
Reference16 articles.
1. P. C. Hughes, Spacecraft Attitude Dynamics (Dover, New York, 2004).
2. G. Avanzini, E. L. de Angelis, and F. Giulietti, “Spin-axis pointing of a magnetically actuated spacecraft,” Acta Astronaut. 94, 493–501 (2014).
3. C. Chasset, S. Berge, et al., “3-axis magnetic control with multiple attitude profile capabilities in the PRISMA mission,” in 57th Int. Astronautical Congress, Valencia, Spain, October 2006, p. IAC-06-C1.2.3. https://doi.org/10.2514/6.IAC-06-C1.2.03
4. A. de Ruiter, “A fault-tolerant magnetic spin stabilizing controller for the JC2Sat-FF mission,” Acta Astronaut. 68, 160–171 (2011). https://doi.org/10.1016/j.actaastro.2010.07.012
5. H. You, Y.-W. Jan, and J.-R. Tsai, “Sun pointing attitude control with magnetic torquers only,” in 57th Int. Astronautical Congress, Valencia, Spain, October 2006, p. IAC-06-C1.2.01. https://doi.org/10.2514/6.IAC-06-C1.2.01
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