Swashplateless control of a rotary-wing UAV using variable RPM and a movable CG

Annual Forum Proceedings - AHS International

Volumn II, Issue , 2006, Pages 878-886

  Gandhi, Farhan ^a,d   Yoshizaki, Yuji ^b   Sekula, Martin K ^c  

^a PENNSYLVANIA STATE UNIVERSITY   (United States)

^b MITSUBISHI HEAVY INDUSTRIES LTD   (Japan)

^c NASA LANGLEY RESEARCH CENTER   (United States)

^d Department of Aerospace Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CYCLIC PITCH CONTROLS; ENGINE CONTROLLERS; OPERATIONAL FLIGHT SPEEDS; ROTARY-WING UAV;

FLIGHT DYNAMICS; FUEL TANKS; HELICOPTERS; ROTORS; SPEED CONTROL; WINGS;

UNMANNED VEHICLES;

EID: 33748441167     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Ormiston, R. A., "Aeroelastic Considerations for Rotorcraft Primary Control with On-Blade Elevons," Proc. of the 57th Annual Forum of the American Helicopter Society, Washington DC, May 9-11, 2001.
2. rd AIAA/ASME/ASCE/ AHS /ASC Structures, Structural Dynamics, and Materials Conference, April 22-25, 2002, Paper No. AIAA-2002-1444.
3. Shen, J., and Chopra, I., "A Parametric Design Study for a Swashplateless Helicopter Rotor with Trailing Edge Flaps," Proc. of the 58th Annual Forum of the American Helicopter Society, Quebec, Canada, June 11-13, 2002.
4. th Annual Forum of the American Helicopter Society, Baltimore, Maryland, June 2004.