ШЕВЧЕНКО, С. В.; БІЛОУС, Д. В. Determination of rational parameter of an aircraft active control system with account the structural flexbility. Proceedings of National Aviation University, [S. l.], v. 18, n. 3-4, p. 86–88, 2021. DOI: 10.18372/2306-1472.18.15405. Disponível em: https://jrnl.nau.edu.ua/index.php/visnik/article/view/15405. Acesso em: 18 may. 2024.