Attitude Control of Flexible Space Vehicles
- 1 June 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (6) , 807-812
- https://doi.org/10.2514/3.50215
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Use of synthetic modes in hybrid coordinate dynamic analysis.AIAA Journal, 1968
- Application of Galerkin's method to the dynamic analysis of structures.AIAA Journal, 1967
- Dynamic analysis of structural systems using component modesAIAA Journal, 1965