Model reduction by Euclidean methods
- 1 November 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance and Control
- Vol. 3 (6) , 555-562
- https://doi.org/10.2514/3.19724
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Appendage modal coordinate truncation criteria in hybrid coordinate dynamic analysisJournal of Spacecraft and Rockets, 1976
- On the Attitude Dynamics of Spinning Deformable SystemsAIAA Journal, 1975