CHÍNH. DYNAMIC MODEL OF THREE JOINTS HELICOPTER ROTOR WITH CONSIDERING NONLINEAR UNSTEADY AERODYNAMICS. Journal of Military Science and Technology, [S. l.], n. 66, p. 199–208, 2020. Disponível em: https://ojs.jmst.info/index.php/jmst/article/view/240. Acesso em: 22 nov. 2024.