Reduced-order models of a large flexible spacecraft
- 1 November 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 12 (6) , 845-850
- https://doi.org/10.2514/3.20490
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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- Modal Truncation for Flexible SpacecraftJournal of Guidance, Control, and Dynamics, 1981
- Modal Cost Analysis for Linear Matrix-Second-Order SystemsJournal of Dynamic Systems, Measurement, and Control, 1980
- Vibration Analysis of Structures by Component Mode SubstitutionAIAA Journal, 1971
- Coupling of substructures for dynamic analyses.AIAA Journal, 1968
- Dynamic analysis of structural systems using component modesAIAA Journal, 1965