Abstract:
The purpose of this research is the mathematical modelling of flight dynamics, stabilizing and control of the Vertical Take-Off and Landing aircraft during its transition...Show MoreMetadata
Abstract:
The purpose of this research is the mathematical modelling of flight dynamics, stabilizing and control of the Vertical Take-Off and Landing aircraft during its transition from vertical to forward flight. The main investigated area is reduced to a two-dimensional case in a vertical plane. The design, analysis and the validation tests have been undertaken on the simulation aerial vehicle in the Matlab/Simulink environment to provide starting point for real flying VTOL model build.
Published in: 2020 7th International Conference on Control, Decision and Information Technologies (CoDIT)
Date of Conference: 29 June 2020 - 02 July 2020
Date Added to IEEE Xplore: 27 November 2020
ISBN Information: