Root / CYBERNETICS AND PHYSICS / Volume 15, 2026, Number 2 / Angular guidance of navigation satellites during passing the singular orbital poses

Angular guidance of navigation satellites during passing the singular orbital poses

Yevgeny Somov, Sergey Somov, Sergey Butyrin, Tatyana Somova, Pavel Kuznetsov

During the flight of a navigation satellite, the solar-terrestrial reference frame is used, based on the unit vectors of directions to the Sun and Earth measured on board, emanating from the mass center of the satellite (object). The problems on attitude control of a navigation satellite when its passing through singular orbital poses are studied in order to ensure predictability of the influence of solar pressure forces on its movement.
CYBERNETICS AND PHYSICS, VOL. 15, NO. 2, 2026, 216–221
https://doi.org/10.35470/2226-4116-2026-15-2-216-221

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