SUDARS, Martins. Development and simulations of aircraft guidance system using a 3–degree‐of‐freedom point mass model. Aviation, [S. l.], v. 13, n. 2, p. 35–43, 2009. DOI: 10.3846/1648-7788.2009.13.35-43. Disponível em: https://journals.vilniustech.lt/index.php/Aviation/article/view/6144. Acesso em: 12 may. 2025.