Dynamics of a cantilever beam attached to a moving base
Author:
Affiliation:
1. Stanford University, Stanford, California
2. Lockheed Missiles and Space Company, Stanford, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.20195
Reference41 articles.
1. Attitude Dynamics of Satellites with Flexible Appendages- A Brief Review
2. Generalized Equations of Motion for the Dynamic Analysis of Elastic Mechanism Systems
3. Dynamic Analysis of Elastic Mechanism Systems. Part I: Applications
4. Dynamic Analysis of Elastic Mechanism Systems. Part II: Experimental Results
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