Feasibility of autonomous orbit keeping with optimal fuel consumption using drag-free CubeSat

نویسندگان

چکیده

Abstract In this paper, the composition of drag-free CubeSat platform was introduced first. Then control strategy orbit keeping proposed. Finally, simulation with scheme Homan transfer compared. By comparing and analyzing fuel consumption track track, it is demonstrated that continuous drag compensation can significantly reduce thruster mass, technology has good advantages in stability.

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ژورنال

عنوان ژورنال: Journal of physics

سال: 2023

ISSN: ['0022-3700', '1747-3721', '0368-3508', '1747-3713']

DOI: https://doi.org/10.1088/1742-6596/2489/1/012011