Coordinate transformation and truncation for rotating spacecraft with flexible appendages
- 1 December 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (12) , 1657-1665
- https://doi.org/10.2514/3.7042
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- A New Method of Solution of the Eigenvalue Problem for Gyroscopic SystemsAIAA Journal, 1974
- Geometric stiffness characteristics of a rotating elastic appendageInternational Journal of Solids and Structures, 1974
- On a combined sturm sequence and inverse iteration technique for eigenproblem solution of spinning structuresInternational Journal for Numerical Methods in Engineering, 1973
- Free vibration analysis of spinning structural systemsInternational Journal for Numerical Methods in Engineering, 1973
- Finite element appendage equations for hybrid coordinate dynamic analysisInternational Journal of Solids and Structures, 1972