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A systematic method of smooth switching LPV controllers design for a morphing aircraft

(in lingua inglese)

In this paper, a systematic method of smooth switching LPV controllers design is explored for a morphing aircraft with a variable wing sweep angle. The LPV model of the morphing aircraft is developed and it can characterize the wing transition phase’s complex behavior.

Articoli tecnico scientifici o articoli contenenti case history
Fonte: Articolo Chinese Journal of Aeronautics, 2015
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