Method for motion control of solar sail spacecraft with reflectivity control devices in case of Earth–Mars flight

The spatial heliocentric flight Earth–Mars of a non-perfectly reflecting solar sail spacecraft is considered. Thin-film control devices located along the perimeter of the solar sail are proposed as a control element. These spatial orientation controls are capable of changing their reflective charact...

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Main Author: Khabibullin, R. M.
Format: Conference Proceeding
Language:English
Subjects:
Algorithms
Control equipment
Earth
Flight
Motion control
Reflectance
Solar sails
Spacecraft
Thin films
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description The spatial heliocentric flight Earth–Mars of a non-perfectly reflecting solar sail spacecraft is considered. Thin-film control devices located along the perimeter of the solar sail are proposed as a control element. These spatial orientation controls are capable of changing their reflective characteristics depending on the voltage applied to them. A mathematical model of the photon pressure on the non-perfectly reflecting surface of the solar sail is described, taking into account the functioning of thin-film reflectivity control devices. An algorithm for generating a program for the nominal motion control of a solar sail spacecraft with and without thin-film control devices is described. The results of the Earth–Mars flight of a solar sail spacecraft have been obtained.
doi_str_mv 10.1063/5.0107853
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source American Institute of Physics:Jisc Collections:Transitional Journals Agreement 2021-23 (Reading list)
subjects Algorithms
Control equipment
Earth
Flight
Motion control
Reflectance
Solar sails
Spacecraft
Thin films
title Method for motion control of solar sail spacecraft with reflectivity control devices in case of Earth–Mars flight
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