Nonlinear Vibrations of Flexible Spacecraft Jointed Composite Appendages: Theory and Experiment
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
Subfield: Control and Systems Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W7129056491
