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Nonlinear Vibrations of Flexible Spacecraft Jointed Composite Appendages: Theory and Experiment

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Year: 2026
Type: article
Source: AIAA Journal
DOI: 10.2514/1.j066294
Authors: Guiqin He, Haichao Gui, Dengqing Cao
Institutions: Beihang University, Harbin Institute of Technology
Language: English

Topic: Dynamics and Control of Mechanical Systems
Subfield: Control and Systems Engineering
Field: Engineering
Domain: Physical Sciences

Open Access status: closed

Funders: National Natural Science Foundation of China, National Key Research and Development Program of China, Fundamental Research Funds for the Central Universities
Awards: 大型柔性航天器姿态运动与结构振动的耦合动力学特性研究, G6414170467, G8178826960
OpenAlex ID: W7129056491
FWCI: 2.843
Cites: 33
Cited by: 1
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