Minimal Thrusters Configuration for Simultaneous Orbit Correction and Reaction Wheels Desaturation for GEO Satellite
The paper considers the problem of the optimal thrusters arrangement aboard a geostationary spacecraft. It is necessary to simultaneously ensure orbit correction and reaction wheels desaturation. A formalization for thrusters optimal arrangement problem is proposed. Examples of the minimal thrusters...
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| Veröffentlicht in: | Cosmic research 2020-09, Vol.58 (5), p.379-392 |
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| container_title | Cosmic research |
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| creator | Okhitina, A. S. Mashtakov, Ya. V. Tkachev, S. S. Shestakov, S. A. Ovchinnikov, M. Yu |
| description | The paper considers the problem of the optimal thrusters arrangement aboard a geostationary spacecraft. It is necessary to simultaneously ensure orbit correction and reaction wheels desaturation. A formalization for thrusters optimal arrangement problem is proposed. Examples of the minimal thrusters arrangement are given, taking into account the given limitations and requirements both in the case of regular operation and in the case of a possible failure of one of the thrusters. The influence of possible installation errors and the center of mass displacement is taken into account. |
| doi_str_mv | 10.1134/S0010952520050081 |
| format | Article |
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| ispartof | Cosmic research, 2020-09, Vol.58 (5), p.379-392 |
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| language | eng |
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| subjects | Astronomy Astrophysics and Astroparticles Astrophysics and Cosmology Desaturation Physics Physics and Astronomy Reaction wheels Satellites Space Exploration and Astronautics Space Sciences (including Extraterrestrial Physics Spacecraft Thrusters |
| title | Minimal Thrusters Configuration for Simultaneous Orbit Correction and Reaction Wheels Desaturation for GEO Satellite |
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