In this study, to develop a mathematical model for a short take-off and vertical landing (STOVL) aircraft dynamics a model system which resembles such aircraft dynamics was studied. The proposed model system uses the thrust of axial fans to hover the whole system in the air. The dynamic equations of the model system are derived and a lift force model is also proposed for a stable landing condition. A simulation model is built and tested for some initial values of the variables and results were evaluated.
Modelling and Simulation of Vertical Landing Dynamics of an Aircraft Based on a Model System
Sustainable aviat.
International Symposium on Unmanned Systems and The Defense Industry ; 2021 ; Washington, DC, DC, USA October 26, 2021 - October 28, 2021
2023-06-28
8 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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