OPTIMUM SATELLITE LAUNCHER TRAJECTORY GUIDED WITH PROPORTIONAL NAVIGATION PLUS GRAVITY COMPENSATION GUIDANCE. مجلة الهندسة, [S. l.], v. 12, n. 04, p. 916–928, 2006. DOI: 10.31026/j.eng.2006.04.04. Disponível em: https://joe.uobaghdad.edu.iq/index.php/main/article/view/2839.. Acesso em: 19 2024.