Enhanced Pitch Angle of Aircraft System Using Fractional Model Reference Adaptive Control Approach. ITEGAM-JETIA, [S. l.], v. 12, n. 59, p. 320–327, 2026. DOI: 10.5935/jetia.v12i59.3437. Disponível em: https://itegam-jetia.org/journal/index.php/jetia/article/view/3437. Acesso em: 22 oct. 2026.