Equations of Motion for Multiple-Rigid-Body Systems via Symbolic Manipulation
Author:
Affiliation:
1. The University of Texas at Austin, Austin, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.57227
Reference15 articles.
1. 'Hooker, W.W. and Margulies, G. "The Dynamical Attitude Equations for an A?Body Satellite/' The Journal of the Astronautical Sciences, Vol.XII, Winter1965, pp.123-128.
2. A set of r dynamical attitude equations for an arbitrary n-body satellite having r rotational degrees of freedom
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