Reduction of large flexible spacecraft models using internal balancing theory
- 1 November 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 7 (6) , 725-732
- https://doi.org/10.2514/3.19919
Abstract
No abstract availableKeywords
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