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Stability issue is one of the elements that need to be considered during the design of an engineering system. We are interested in instabilities in landing gears during ground manoeuvre and the methods presented in the journal show how to select structural parameters in order to limit the possible occurrence of instabilities in the stated aircraft systems.

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This page is a summary of: Enhanced Evolutionary-Based Optimization Techniques Applied to a Nonlinear Landing Gear Design Problem, Journal of Aircraft, September 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c035198.
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