Design of Robust H∞ Combined with PID Controller Using Fuzzy Logic for a Missile Autopilot. Advances in Military Technology, [S. l.], v. 19, n. 1, p. 41–53, 2024. DOI: 10.3849/aimt.01831. Disponível em: https://www.aimt.cz/index.php/aimt/article/view/1831.. Acesso em: 25 aug. 2024.