Geodesic
Modelling of a satellite mockup angular motion on the air bearing with the one-axis magnetic attitude control
Matematičeskoe modelirovanie, Tome 31 (2019) no. 11, pp. 36-46.

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Angular motion of the mockup of the satellite attitude control system on the air bearing is considered. The general purpose of the work is to verify the one-axis magnetic attitude control algorithm. This control is designed to maintain the satellite solar panels attitude towards the Sun. Specific mockup motion patterns are found. These patterns allow the comparison between the ground-based control performance results and its expected inflight operation. Asymptotically stable precession and near planar motion are outlined. Mathematical modelling is performed for these patterns. Their applicability for the laboratory experiments is shown.
Keywords: air bearing, angular motion, magnetic attitude control, one-axis stabilization. 
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     title = {Modelling of a satellite mockup angular motion on the air bearing with the one-axis magnetic attitude control},
     journal = {Matemati\v{c}eskoe modelirovanie},
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M. Yu. Ovchinnikov; D. S. Roldugin; R. A. Borges; C. Cappelletti; S. Battistini. Modelling of a satellite mockup angular motion on the air bearing with the one-axis magnetic attitude control. Matematičeskoe modelirovanie, Tome 31 (2019) no. 11, pp. 36-46. http://geodesic.mathdoc.fr/item/MM_2019_31_11_a2/

[1] D. S. Ivanov et al, “Testing of attitude control algorithms for microsatellite “Chibis-M” at laboratory facility”, Journal of Computer and Systems Sciences International, 51:1 (2012), 106–125 | DOI | Zbl

[2] W. Haeussermann, H. Kennel, “A Satellite Motion Simulator”, Automatica, 5:12 (1960), 22–25; 90–91

[3] M. A. Peck et al, “An Airbearing-Based Testbed for Momentum Control Systems and Spacecraft Line of Sight”, Adv. Astronaut. Sci., 114 (2003), AAS 03-127

[4] J. Prado et al, “Three-axis air-bearing based platform for small satellite attitude determination and control simulation”, J. Appl. Res. Technol., 3:3 (2005), 222–237

[5] I. Ishioka et al., “HIL Testing of the B-dot Attitude Control Law”, III IAA Latin American CubeSat Workshop (Ubatuba, 2018), IAA-BR-18-09-05

[6] M. Yu. Ovchinnikov et al, “New one-axis one-sensor magnetic attitude control theoretical and in-flight performance”, Acta Astronaut., 105:1 (2014), 12–16 | DOI

[7] S. O. Karpenko et al, “One-axis attitude of arbitrary satellite using magnetorquers only”, Cosm. Res., 51:6 (2013), 478–484 | DOI

[8] M. Yu. Ovchinnikov et al, “Geomagnetic field models for satellite angular motion studies”, Acta Astronaut., 144 (2018), 171–180 | DOI | MR