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 (archive), [S. l.], v. 18, n. 3-4, p. 86–88, 2021. DOI: 10.18372/2306-1472.18.15405. Disponível em: http://jrnl.kai.edu.ua/index.php/visnik/article/view/15405. Acesso em: 14 jun. 2026.