Equilibrium attitude transitions of a three-rotor gyrostat in a circular orbit.

DOI10.2514/3.6775zbMath0251.70018OpenAlexW2054909768MaRDI QIDQ5664857

Atanas A. Anchev

Publication date: 1973

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.6775

Mathematics Subject Classification ID

Orbital mechanics (70M20) Dynamics of a rigid body and of multibody systems (70E99)

Related Items (5)

A time-optimal control synthesis for a nonlinear pendulum ⋮ Bifurcation in a time-optimal problem for a second-order nonlinear system ⋮ Properties of the time-optimal feedback control for a pendulum-like system ⋮ On the equilibrium configuration of a particular three-body system ⋮ Dispersal curve properties in the time minimization problem for a second-order nonlinear system

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