1.
Шевченко СВ, Білоус ДВ. Determination of rational parameter of an aircraft active control system with account the structural flexbility. Proceedings of National Aviation University [Internet]. 2021 May 5 [cited 2025 Jan. 31];18(3-4):86-8. Available from: https://jrnl.nau.edu.ua/index.php/visnik/article/view/15405