Equivalent Beam Model and Improved Structure Design of Large Space Antenna Truss With Geometric Nonlinearity
Author:
Affiliation:
1. Department of Engineering Mechanics, MOE Key Laboratory of Hydrodynamics, State Key Laboratory of Ocean Engineering, Shanghai Jiao Tong University , Shanghai 200240, China
Abstract
Funder
National Natural Science Foundation of China
Publisher
ASME International
Subject
Applied Mathematics,Mechanical Engineering,Control and Systems Engineering,General Medicine
Link
https://asmedigitalcollection.asme.org/computationalnonlinear/article-pdf/18/5/051003/6995759/cnd_018_05_051003.pdf
Reference23 articles.
1. A Review on Large Deployable Structures for Astrophysics Missions;Acta Astronaut.,2010
2. Overview of the Innovative Space-Based Radar Antenna Technology Program;J. Spacecr. Rockets,2011
3. Design and Analysis of a Scissors Double-Ring Truss Deployable Mechanism for Space Antennas;Aerosp. Sci. Technol.,2019
4. Nonlinear Dynamic Analysis Near Resonance of a Beam-Ring Structure for Modeling Circular Truss Antenna Under Time-Dependent Thermal Excitation;Aerosp. Sci. Technol.,2019
5. Nonlinear Attitude Control of a Spacecraft With Distributed Actuation of Solar Arrays;J. Guid. Control Dynam.,2019
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