The accretion of ice layers on wings and control surfaces modifies their lift and drag and, consequently, alters performance and controllability of the aircraft. In this paper we propose a combined unknown input observers and control allocation framework to design icing diagnosis filters and accommodate icing for an overactuated automated aircraft.
An unknown input observer based control allocation scheme for icing diagnosis and accommodation in overactuated UAVs
CRISTOFARO, ANDREA;
2016-01-01
Abstract
The accretion of ice layers on wings and control surfaces modifies their lift and drag and, consequently, alters performance and controllability of the aircraft. In this paper we propose a combined unknown input observers and control allocation framework to design icing diagnosis filters and accommodate icing for an overactuated automated aircraft.File in questo prodotto:
Non ci sono file associati a questo prodotto.
I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
