Satellite dynamics due to gravity and constant torques

DOI10.1134/S1064230716060058zbMath1384.93016MaRDI QIDQ1745753

A. D. German, Vasily A. Sarychev, Sergey A. Gutnik

Publication date: 18 April 2018

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

zbMATH Keywords

gravitydynamicscircular orbitalgebraic methodscentral Newtonian force fieldconstant torquesdiscriminant hypersurfacesrotational motion of a satellite

Mathematics Subject Classification ID

Application models in control theory (93C95) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (1)

Implementation of the orbital 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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• Dynamics of a gyrostat satellite subjected to the action of gravity moment. Equilibrium attitudes and their stability
• Influence of constant torque on equilibria of satellite in circular orbit
• Application of Computer Algebra Methods to Investigation of Influence of Constant Torque on Stationary Motions of Satellite

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