What is it about?
The frequency response of an aircraft is usually investigated using linear methods. We propose a new method to do this using nonlinear techniques.
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This page is a summary of: Frequency-Domain Bifurcation Analysis of a Nonlinear Flight Dynamics Model, Journal of Guidance Control and Dynamics, September 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g005197.
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