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This article is cited in 3 scientific papers (total in 3 papers)
Mathematical modelling of the dynamics of a satellite equipped with atmosphere-breathing electric propulsion system
M. Yu. Ovchinnikova, A. D. Guermanb, Y. V. Mashtakova, D. S. Roldugina a Keldysh Institute of Applied Mathematics of RAS
b University of Beira Interior, Portugal
Abstract:
Simulation of a satellite motion on an extremely low Earth orbit with approximately 175
km altitude is performed. The satellite is equipped with the air-breathing electric propulsion system that compensates the aerodynamic drag. Simulation of the controlled angular
motion is performed with major disturbance factors. Namely, errors in the mass distribution, propulsion system thrust direction and position errors, and winds in the atmosphere.
Control system power consumption in different operational modes is estimated.
Keywords:
air-breathing propulsion, electric propulsion, extremely low orbit.
Received: 30.08.2021 Revised: 30.08.2021 Accepted: 04.10.2021
Citation:
M. Yu. Ovchinnikov, A. D. Guerman, Y. V. Mashtakov, D. S. Roldugin, “Mathematical modelling of the dynamics of a satellite equipped with atmosphere-breathing electric propulsion system”, Matem. Mod., 33:11 (2021), 18–38; Math. Models Comput. Simul., 14:3 (2022), 452–465
Linking options:
https://www.mathnet.ru/eng/mm4332 https://www.mathnet.ru/eng/mm/v33/i11/p18
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