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Hybrid-polynomial-based optimization for buffer mechanism of asteroid probe with uncertainty

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Year: 2025
Type: article
Source: Aircraft Engineering and Aerospace Technology
DOI: 10.1108/aeat-06-2025-0235
Authors: Hongyu Wu, Penghui Yao, Hui Wang, Jiahao Ding, Maolin Liao, Hengrui Zhang, Shaoze Yan
Institutions: University of Science and Technology Beijing, China Academy of Launch Vehicle Technology, State Key Laboratory of Tribology, Tsinghua University
Language: English

Topic: Advanced Multi-Objective Optimization Algorithms
Subfield: Computational Theory and Mathematics
Field: Computer Science
Domain: Physical Sciences

Open Access status: closed

Funders: National Natural Science Foundation of China, Fundamental Research Funds for the Central Universities
Awards: G3467888762, G6671982165
OpenAlex ID: W4415296165
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Cites: 15
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