Gravitational stabilization of a satellite using a movable mass

DOI10.1016/j.jappmathmech.2012.09.007zbMath1423.70057OpenAlexW2029429410MaRDI QIDQ2331270

S. P. Bezglasnyi, Vladimir S. Aslanov

Publication date: 25 October 2019

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jappmathmech.2012.09.007

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Orbital mechanics (70M20) Control/observation systems governed by ordinary differential equations (93C15)

Related Items

Nonlinear Stability Analysis of Relative Equilibria of a Solid Carrying a Movable Point Mass in the Central Gravitational Field ⋮ Approximate equations of rotational motion of a rigid body carrying a movable point mass ⋮ Threshold absolute value of a relay control when time-optimally bringing a satellite to a gravitationally stable position

Cites Work

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• On the motion of a satellite about its center of mass under the action of gravitational moments