Synthesis of dynamics of nanosatellites with variable inertial-mass parameters-Reference-Cited by-同舟云学术

Synthesis of dynamics of nanosatellites with variable inertial-mass parameters

Published:2022-03-01 Issue:1 Volume:2182 Page:012049
ISSN:1742-6588
Container-title:Journal of Physics: Conference Series
language:
Short-container-title:J. Phys.: Conf. Ser.

Author:

Doroshin A V,Eremenko A V

Abstract

Abstract The work considers the dynamics of a composite nanosatellite with variable inertial-mass parameters. The nanosatellite consists of two units connected to each other by flexible rods, a main unit (nanosatellite body) and a mobile unit. A passive system for stabilizing the rotational motion of a composite nanosatellite is considered, which uses a mobile unit as a motion control actuating element.

Publisher

IOP Publishing

Subject

General Physics and Astronomy

Link

https://iopscience.iop.org/article/10.1088/1742-6596/2182/1/012049/pdf

Reference5 articles.

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2. Attitude dynamics of nanosatellite with a module on retractable beams;Aslanov;J. Phys.: Conf. Ser.,2019

3. Attitude control of nanosatellite with single thruster using relative displacements of movable unit;Doroshin,2020

4. A survey on moving mass control technology;Li;Aerosp Sci Technol,2018

5. Algorithms of stabilization of a spacecraft with flexible elements;Ovchinnikov;J Comput Syst Sci Int,2019

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