Roll Control for a Micro Air Vehicle Using Active Wing Morphing
Author:
Affiliation:
1. University of Florida
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-5347
Reference18 articles.
1. M.AmprikidisandJ.E.Cooper,“Developmentof Smart Spars for Active Aeroelastic Structures,” AIAA2003-1799,2003.
2. J.Blondeau,J. RichesonandD.J.Pines,“Design, Development and Testing of a Morphing Aspect Ratio WingusinganInflatableTelescopicSpar,”AIAA-2003-1718.
3. J. Bowman, B. Sanders and T. Weisshar, “Evaluating the Impact of Morphing Technologies on Aircraft Performance,”AIAA-2002-1631,2002.
4. D.Cadogan,T.Smith,R.LeeandS.Scarborough, “Inflatable and Rigidizable Wing Components for UnmannedAerialVehicles,”AIAA-2003-1801,2003.
5. C.E.S. Cesnik and E.L. Brown, “Active Warping Control of a Joined-Wing Airplane Configuration,” AIAA-2003-1716,2003.
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