Equilibrium attitude transitions of a three-rotor gyrostat in a circular orbit.
Author:
Affiliation:
1. Bulgarian Academy of Sciences, Sofia, Bulgaria
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6775
Reference5 articles.
1. Stability of orbiting gyrostats in the elementary cases
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