A set of r dynamical attitude equations for an arbitrary n-body satellite having r rotational degrees of freedom
- 1 July 1970
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (7), 1205-1207
- https://doi.org/10.2514/3.5873
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- On the Derivation of Equations of MotionJournal of the Society for Industrial and Applied Mathematics, 1965