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Nonlinear Model Reduction for Aeroelastic Control of Flexible Aircraft Described by Large Finite-Element Models (2014)

First Author: Wang Y

Attributed to: Nonlinear Flexibility Effects on Flight Dynamics and Control of Next-Generation Aircraft funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.2514/6.2014-0842

Publication URI: http://dx.doi.org/10.2514/6.2014-0842

Type: Conference/Paper/Proceeding/Abstract