Military vehicles are generally equipped with hydro-gas suspension systems that exhibit better shock-absorbing capability over drastic dynamic environments compared to linear suspension. In order to implement suspension semi-active/active control in the future, it is required to develop the mathematical model of the vehicle using non-linear state space approach by incorporating the hydro-gas suspension trailing arm dynamics in the governing equations of motion. The present study formulates the non-linear state space approach which simulates single station ride dynamics of military vehicles. Incorporating the developed trailing arm kinematics and non-linear suspension characteristics, non-linear state space approach has been used to formulate the sprung and unsprung mass governing equations of motion. The multi-body dynamics model for the single station is established in MSC.ADAMS in order to validate the non-linear state space model. The mathematical model is solved using MATLAB and compares well with the multi-body model simulations. The entire military vehicle non-linear state space model can also be developed which would be suitable for carrying out vehicle dynamics control studies with active or semi-active suspension systems.


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    Titel :

    Non-linear State Space Formulation Simulating Single Station Ride Dynamics of Military Vehicle


    Weitere Titelangaben:

    Lect.Notes Mechanical Engineering


    Beteiligte:
    Dutta, Subashisa (Herausgeber:in) / Inan, Esin (Herausgeber:in) / Dwivedy, Santosha Kumar (Herausgeber:in) / Banerjee, Saayan (Autor:in) / Balamurugan, V. (Autor:in) / Krishna Kumar, R. (Autor:in)


    Erscheinungsdatum :

    12.10.2020


    Format / Umfang :

    18 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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