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Towards development of a nonlinear and flexible multi-body helicopter inceptor model: a resonant frequency tuning study. (2021)

First Author: Yap E

Attributed to: Aircraft Active Inceptor Dynamics under Vibration Loads funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.2514/6.2021-1266

Publication URI: http://dx.doi.org/10.2514/6.2021-1266

Type: Conference/Paper/Proceeding/Abstract