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Flight Test Design and Nonlinear Model Identification for Landing Gear Aerodynamics.

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Bibliographic Details
Title: Flight Test Design and Nonlinear Model Identification for Landing Gear Aerodynamics.
Authors: Cai, Xiangqun1 (AUTHOR), Lei, Xiaoyong2 (AUTHOR) leixy@buaa.edu.cn, Dai, Shuling3 (AUTHOR), Li, Weiqi4 (AUTHOR)
Source: International Journal of Aeronautical & Space Sciences. Mar2025, Vol. 26 Issue 2, p800-814. 15p.
Database: Academic Search Ultimate
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Description
ISSN:2093274X
DOI:10.1007/s42405-024-00786-6