The Direct Path Method for deriving the dynamic equations of motion of a multibody flexible spacecraft with topological tree configuration
- 5 August 1974
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Results of flexible spacecraft attitude control studies utilizing hybrid coordinatesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970