Component Model Parameter Updating for Landing Gear Linkages with Flexible Joints
Author:
Affiliation:
1. Department of Aerospace Engineering, Ryerson University, Toronto, Ontario M5B 2K3, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053690
Reference37 articles.
1. Coupling of substructures for dynamic analyses.
2. A hybrid method of component mode synthesis
3. Improved Component-Mode Representation for Structural Dynamic Analysis
4. Model Updating In Structural Dynamics: A Survey
5. Analytical model improvement using frequency response functions
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