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Numerical continuation applied to landing gear mechanism analysis

Research output: Working paperWorking paper and Preprints

Original languageEnglish
Publication dateNov 2010
StatePublished

Abstract

A method of investigating quasi-static mechanisms is presented and applied to an overcentre mechanism and to a nose landing gear mechanism. The method uses static equilibrium equations along with equations describing the geometric constraints in the mechanism. In the spirit of bifurcation analysis, solutions to these steady-state equations are then continued numerically in parameters of interest. Results obtained from the bifurcation method agree with the equivalent results obtained from two overcentre mechanism dynamic models (one state-space and one multibody dynamic model), whilst a considerable computation time reduction is demonstrated with the overcentre mechanism. The analysis performed with the nose landing gear model demonstrates the flexibility of the continuation approach, allowing conventional model states to be used as continuation parameters without a need to reformulate the equations within the model. This flexibility, coupled with the computation time reductions, suggests that the bifurcation approach has potential for analysing complex landing gear mechanisms.

Additional information

Sponsorship: This research was supported by an Engineering and Physical Sciences Research Council (EPSRC) Case Award grant in collaboration with Airbus in the UK.

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  • Preprint

    Preprint (usually an early version) , 4 MB, PDF-document

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