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Control of a flexible wing aircraft

2013
Modern aircrafts are becoming lighter and more flexible to meet fuel efficiency, endurance and other requirements. The structural modes therefore occur at lower frequencies and there is an increased coupling between the structural and rigid body modes.
Graafmans, J.A.J.   +2 more
openaire   +1 more source

Flexible Skins for Morphing Aircraft

Journal of Intelligent Material Systems and Structures, 2010
openaire   +1 more source

Adaptive fault-tolerant boundary control for a flexible aircraft wing with input constraints

Aerospace Science and Technology, 2019
Shiqi Gao, Zhijie Liu
exaly  

Disturbance observer design and vibration control for a flexible aircraft wing

Transactions of the Institute of Measurement and Control, 2018
Yuanyuan Zhang, Jinkun Liu, Wei He
exaly  

Modeling and simulation of mass-actuated flexible aircraft for roll control

Aerospace Science and Technology, 2020
Xiaoming Wang
exaly  

Nonlinear Dynamic Inversion of a Flexible Aircraft

IFAC-PapersOnLine, 2016
Ryan James Caverly   +2 more
exaly  

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