This study is aimed at developing a simplified virtual model capable of simulating the dynamic behavior of a fixed-wing aircraft by applying the multibody approach. The case of an aircraft with simplified aerodynamics, an axial thrust, and without control surfaces is considered. After modeling the aerodynamic actions following a Lagrangian approach, the equations of motion are analytically derived and numerically implemented in a MATLAB computer code to develop a virtual model capable of simulating the dynamic behavior of the aircraft. Finally, the numerical results found are presented and a discussion on the numerical results is provided, paying attention to the Cessna 172 Skyhawk, which is considered as the case study.


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    Titel :

    Multibody Modeling and Dynamical Analysis of a Fixed-Wing Aircraft


    Weitere Titelangaben:

    Lect. Notes in Networks, Syst.


    Beteiligte:
    Karabegović, Isak (Herausgeber:in) / Kovačević, Ahmed (Herausgeber:in) / Mandžuka, Sadko (Herausgeber:in) / Curcio, Maria (Autor:in) / Pappalardo, Carmine Maria (Autor:in) / Guida, Domenico (Autor:in)

    Kongress:

    International Conference “New Technologies, Development and Applications” ; 2022 ; Sarajevo, Bosnia and Herzegovina June 23, 2022 - June 25, 2022



    Erscheinungsdatum :

    26.05.2022


    Format / Umfang :

    8 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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