Multi-functional morphing trailing edge device for control of all-composite, all-electric flying wing aircraft

8th AIAA Aviation Technology, Integration and Operations (ATIO) Conference

Volumn , Issue , 2008, Pages

  Wildschek, Andreas ^a   Grünewald, Michael ^a   Maier, Rudolf ^a   Steigenberger, Josef ^a   Judas, Michael ^a   Deligiannidis, Nikolaos ^a   Aversa, Nicky ^b  

^a AIRBUS GROUP INNOVATIONS   (Germany)

^b AIRBUS   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE WING; AIRCRAFT DESIGN; AIRCRAFT MOVEMENTS; ALL-COMPOSITE AIRCRAFT; ALL-ELECTRIC AIRCRAFT; ELECTRIC ACTUATION SYSTEM; FLAP DEFLECTION; FLIGHT CONTROL; FLYING WINGS; FLYING-WING AIRCRAFT; FUEL EFFICIENCY IMPROVEMENT; FULL CONTROL; HIGH POTENTIAL; LOAD ALLEVIATION; LOAD CONTROL; LONG RANGE TRANSPORT; LONG TERM; MORPHING; MULTI-FUNCTIONAL; MULTI-OBJECTIVE CONTROL; THREE AXES; TRAILING EDGES;

AIRCRAFT MANUFACTURE; AIRFRAMES; AVIATION; CONTROL SURFACES; DESIGN; FLIGHT CONTROL SYSTEMS; TRANSPORT AIRCRAFT;

AIRCRAFT CONTROL;

EID: 77958473365     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

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3. BRITT, R., JACOBSON, S., AND ARTHURS, T., "Aero-servo-elastic Analysis of the B-2 Bomber," Journal of Aircraft, Vol. 37, No. 5, September/October 2000.
4. MYHRA, D., "The Horten Ho 9/Ho 229," Schiffer Publishing Ltd., 2004.
5. WILDSCHEK, A., MAIER, R., JATEGAONKAR, R., AND BAIER, H., "Augmentation of active wing bending control with a supplementary adaptive feed-forward control algorithm," EUCASS 2007-2nd European Conference For Aerospace Sciences, Brussels, Belgium, 01-06. July, 2007.
6. United States Patent US6276641.
7. MÜLLER, G., GRÜNEWALD, M., MÖSER, C., AND STEIGENBERGER, J., "Variable Flügelstruktur," DGLR Jahrbuch 1999.