Identification of Lateral-Directional Aerodynamic Parameters for Aircraft Based on a Wind Tunnel Virtual Flight Test

In the early stages of aircraft design, a scaled model of the aircraft is installed in a wind tunnel for dynamic semi-free flight to approximate real flight, and the test data are then used to identify the aerodynamic parameters. However, the absence of the translational motion of the test model mak...

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Detalhes bibliográficos

Principais autores:	Shang Tai, Lixin Wang, Yanling Wang, Shiguang Lu, Chen Bu, Ting Yue
Formato:	Artigo
Idioma:	Inglês
Publicado em:	MDPI AG 2023-04-01
Colecção:	Aerospace
Assuntos:	scaled model wind tunnel virtual flight test parameter identification output error method flight control law flight dynamics
Acesso em linha:	https://www.mdpi.com/2226-4310/10/4/350
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