Rolling Active Control for an Aircraft of Seamless Aeroelastic Wing
Author:
Affiliation:
1. Cranfield University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2197
Reference15 articles.
1. Andersen,G.Forster,E. andKolonay,R. (1997) `Multiple control surface utilization inactive aeroelastic wing technology',Journal of Aircraft,Vol.34,No.4,pp.552-531.
2. Armanios,E.A. and Badir,A.M.(1995) `Free vibrationanalysis of anisotropic thin walledclosed-crosssectionBeams',AIAAJournal,Vol. 33,pp. 1905-1910.
3. Boehm,L.B.,Flick,P. and Sanders,M.B.(2000)'Static aeroelastic response predictions of the active aeroelastic wing(AAW) flight research vehicle', 42ndAIAA/ASME/ASCE/AHS/ASCStructures, Structural Dynamics,and MaterialsConference, No.AIAA-2001-1372,Seattle,WA.
4. Cook,M.V. 2007 'Flight dynamics priciples',Butterworth-Heinemann,pp.174-206.
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