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Authors
Zhang, Yu-Hao
Tang, Haifeng
Xing, Shichao
Dai, Ming
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Funding
Funding for this research was provided by:
the Scientific Research Projects of Colleges and Universities in Anhui Province (Grant No. 2024AH040230)
the State Key Laboratory of Mechanics and Control for Aerospace Structures (Grant No. MCAS-E-0325Y01)
the Scientific Research Plan Project of Tongling University (Grant No. 2023tlxyptZD06)
Dai acknowledges the National Natural Science Foundation of China (Grant No. 12572077)
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Article History
Received: 16 October 2025
Revised: 7 March 2026
Accepted: 30 March 2026
First Online: 13 April 2026
Declarations
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: The authors declare no competing interests.
