[1]
Шевченко, С.В. and Білоус, Д.В. 2021. Determination of rational parameter of an aircraft active control system with account the structural flexbility. Proceedings of National Aviation University. 18, 3-4 (May 2021), 86–88. DOI:https://doi.org/10.18372/2306-1472.18.15405.