Dynamic Modeling and Theoretical Analysis of Planar Nonlinear Vibrations of an Articulated Hoop Truss Antenna

Author:

Fang Bo12ORCID,Wang Yilong12ORCID,Wu Yi3ORCID,Han Jae-Hung2ORCID,Cao Dengqing1

Affiliation:

1. School of Astronautics, Harbin Institute of Technology, Harbin 150001, P. R. China

2. Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 34141, Korea

3. IoT Thrust, The Hong Kong University of Science, and Technology (Guangzhou), Guangzhou 510000, P. R. China

Abstract

The dynamic behaviors of large-scale hoop truss antennas (HTAs) are significantly influenced by the nonlinear torque transmission properties of flexible hinges. Due to the nonlinearity of the hinge, the HTA can be easily excited to exhibit internal resonances that result in the energy exchange between the adjacent two or three modes. This paper focuses on the 3:1 internal resonant responses of an articulated HTA induced by the nonlinearity of the hinge. The analytical modes are obtained by using the global mode method (GMM) and are validated by finite element method (FEM). Then the partial differential equations (PDEs) of planar motions are discretized into ordinary differential equations (ODEs) by Galerkin’s technique. The multiple time scale method is employed to obtain the four-dimensional modulation equations of the HTA with primary and 3:1 internal resonance. By using the Newton–Raphson iteration and the pseudo arclength continuation, frequency–response and force–response curves are obtained to investigate the theoretical steady-state vibrations of the HTA. Moreover, the influence of the cubic spring stiffness, damping, and external excitation amplitude on the system’s nonlinear dynamic behaviors are investigated. The numerical simulation reveals that the articulated multi-beam hoop structure exhibits typical nonlinear phenomena such as hardening-spring type characteristic, jumps, bi-stability, and double peaks. The research findings contribute to the reliable structural design and vibration control of the articulated hoop truss antenna.

Funder

National Key Research and Development Program of China

National Natural Science Foundation of China

China Scholarship Council

Advanced Research Project on Civil Space Technology in China

Publisher

World Scientific Pub Co Pte Ltd

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