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