Studying the possibility of ensuring the stabilization accuracy characteristics of an advanced spacecraft for remote sensing of the Earth

DOI10.1134/S1064230718040123zbMath1401.93151OpenAlexW2888726156WikidataQ129335802 ScholiaQ129335802MaRDI QIDQ1994814

A. V. Sumarokov, V. N. Platonov

Publication date: 2 November 2018

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

Full work available at URL: https://doi.org/10.1134/s1064230718040123

zbMATH Keywords

remote sensing satellitesingle-gimbal control momentum gyrosstabilization accuracy

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) Control of mechanical systems (70Q05)

Related Items (2)

Controlling a satellite using single-gimbal control moment gyroscope during their spinning and braking ⋮ Application of generalized Butterworth polynomials for stabilization of the equilibrium position of a space station

Cites Work

• Stabilization of a wheels carrying communication satellite without angle and angular velocity sensors
• On an adaptive control system for angular motion of a communication satellite

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