Appendage modal coordinate truncation criteria in hybrid coordinate dynamic analysis
Author:
Affiliation:
1. Columbia University, New York, New York
2. National Aerospace Laboratory, Tokyo, Japan
3. Hughes Aircraft Company, Canoga Park, Calif
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.27933
Reference9 articles.
1. Dynamic analysis of structural systems using component modes
2. Eigenvalues and eigenvectors for hybrid coordinate equations of motion for flexible spacecraft
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