Modal analysis of a deployable truss using the finite element method

• 1 September 1984
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
• Vol. 21  (5) , 468-472
• https://doi.org/10.2514/3.25682

Abstract

Keywords

• FINITE ELEMENT METHOD
• MODAL ANALYSIS