SIMULATION, PARAMETER IDENTIFICATION AND CONTROL SYSTEM DESIGN OF AN AIRCRAFT USING UNIFIED MATHEMATICAL MODEL. ASEAN Engineering Journal, [S. l.], v. 3, n. 1, p. 5–27, 2013. DOI: 10.11113/aej.v3.15381. Disponível em: https://journals.utm.my/aej/article/view/15381.. Acesso em: 6 apr. 2025.