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

DOI10.1134/S1064230720030065zbMath1453.93178OpenAlexW3005110112MaRDI QIDQ786176

A. I. Ignatov

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/s1064230720030065

zbMATH Keywords

angular momentum of gyro systemartificial satellite stabilizationsolar orientation mode

Mathematics Subject Classification ID

Application models in control theory (93C95) Lyapunov and other classical stabilities (Lagrange, Poisson, (L^p, l^p), etc.) in control theory (93D05)

Cites Work

• Spacecraft attitude control with simultaneous unloading of the angular momentum of inertial actuators
• Implementation of the orbital orientation mode of an artificial satellite of the Earth without accumulation of the angular momentum of the gyro system
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