This report discusses the development of a simulation model of an aircraft landing gear describing its typical non-linear behaviour. The development of the design tool -which correlates the actual design parameters with the performance of the gear- is a part of the research project that investigates the estimation of the nonlinear dynamical system, which an aircraft landing gear is. This project is a joint effort by the Eindhoven University of Technology and DAF Special Products.

    The non-linear parts of the simulation model are implemented in the general purpose multi body program DADS, which is based on time integration procedures.


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    Title :

    TIRE MODELS IN AIRCRAFT LANDING GEAR SIMULATION


    Contributors:

    Published in:

    Vehicle System Dynamics ; 21 , sup1 ; 108-115


    Publication date :

    1992-01-01




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




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