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

Publisher Website

1 April 1973

journal article
Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal

Vol. 11 (4) , 467-472
https://doi.org/10.2514/3.6775

Abstract

No abstract available

This publication has 1 reference indexed in Scilit:

Stability of orbiting gyrostats in the elementary cases
Archive of Applied Mechanics, 1970