A mathematical model for landing a single-rotor helicopter with a wheeled chassis in standard conditions and special cases

Abstract

At the present stage of development of the design of modern aviation equipment, in conditions of fierce rivalry, there are obvious trends to reduce the design time, to lower the final cost, as well as to increase the safety of the product being designed. One of the ways to solve this problem, along with increasing the functionality of the calculation software, is to reduce the volume of certification work by replacing full - scale stand and flight tests with mathematical modeling.