Unscented transformation method for robustness verification of helicopter flight control system

In response to the large computational load and extended processing time associated with the Monte Carlo method in the robustness verification of helicopter flight control systems, this paper proposes an unscented transformation method for such verification. This method employs particle swarm optimi...

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Bibliographic Details
Main Authors: LIU Changqi, LI Aijun, DUAN Guangzhan, LI Zuo
Format: Article
Language:Chinese
Published: Editorial Department of Advances in Aeronautical Science and Engineering 2025-06-01
Series:Hangkong gongcheng jinzhan
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Online Access:http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2023252
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