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. DOI: 10.54939/1859-1043.j.mst.66.2020.199-208. Disponível em: https://jmst.mod.gov.vn/index.php/jmst/article/view/240. Acesso em: 12 mar. 2026.