Implementation of the orbital orientation mode of an artificial satellite of the Earth without accumulation of the angular momentum of the gyro system

DOI10.1134/S1064230719060066zbMath1448.93240OpenAlexW4251069229MaRDI QIDQ786109

A. I. Ignatov, V. V. Sazonov

Publication date: 12 August 2020

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230719060066

zbMATH Keywords

artificial satellitegyro systemorbital orientation mode

Mathematics Subject Classification ID

Application models in control theory (93C95) Linearizations (93B18)

Related Items (1)

Stabilization of the solar orientation mode of an artificial satellite of the Earth without accumulation of the angular momentum of the gyro system

Cites Work

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• Spacecraft attitude control with simultaneous unloading of the angular momentum of inertial actuators
• Satellite dynamics due to gravity and constant torques
• Space Station attitude control and momentum management - A nonlinearlook

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