Open AccessDevelopment of the mathematical model for the tilt-rotor aircraft
Author(s) -
Konstantin S. Lelkov,
D. V. Ulyanov,
D A Surkov,
A N Ushakov
Publication year - 2021
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1925/1/012041
Subject(s) - aerodynamics , tilt (camera) , aerospace engineering , rotor (electric) , flight dynamics , euler's formula , computer science , control theory (sociology) , engineering , mechanical engineering , mathematics , artificial intelligence , mathematical analysis , control (management)
In this paper, main challenges of the urban air mobility concept are discussed and comparison of the different aircraft types, capable of performing vertical take-off and landing for compliance to the urban aerial mobility concept is provided. The mathematical model for the tilt-rotor aircraft is derived by the Newton-Euler method. This model takes into account all the forces and moments applied to the aircraft. Aerodynamic characteristics for the developed aircraft were obtained using virtual aerodynamic blowing method. Simulation results of the tilt-rotor aircraft motion on the various flight stages, including vertical take-off and landing, horizontal flight and transition stages are presented.