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  • Dynamics simulation of changing diameter for a flexible diameter-variable wheel of lunar rover

    Paper number

    IAC-11,A5,1,10,x10995

    Author

    Dr. Zhe Wang, Beijing Institute of Astronautical Systems Engineering, China

    Coauthor

    Prof. Feng Gao, Beihang University, China

    Coauthor

    Dr. Peng Sun, Beihang University, China

    Coauthor

    Dr. Ying Cui, Beihang University, China

    Year

    2011

    Abstract
    Considering the nonlinear deformation of a patented Diameter-Variable Wheel of lunar rover on changing diameter, a FE(Finite Element) model which taking geometric stiffness into account was built through FEMBS(the interface with Finite Element software--Ansys and Multibody System software--Simpack). Based on continuous impact theory, rigid-flexible coupling dynamics simulation of the Diameter-Variable Wheel with six-flexible bodies was carried out by adding moved markers. Then two simulation models were set up respectively for different ways of changing diameter, and the comparative results were given. These studies provide the basis for fatigue life analysis and load verification.
    Abstract document

    IAC-11,A5,1,10,x10995.brief.pdf

    Manuscript document

    IAC-11,A5,1,10,x10995.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.