메뉴 건너뛰기




Volumn II, Issue , 2006, Pages 877-885

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

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL STRATEGIES; ENGINE CONTROLLER; LATERAL DIRECTIONS; OPERATIONAL FLIGHTS; PITCH ATTITUDE; PITCHING MOMENTS; PROPULSIVE FORCES; ROTOR THRUST;

EID: 84884302165     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (4)

References (4)
  • 1
    • 84884298293 scopus 로고    scopus 로고
    • 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
    • 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.
    • (2001)
    • Ormiston, R.A.1
  • 2
    • 0036079068 scopus 로고    scopus 로고
    • Actuation Requirements for a Swashplateless Helicopter Control System with Trailing-Edge Flaps
    • Proc. of the 43rd AIAA/ASME/ASCE/ AHS /ASC Structures, Structural Dynamics, and Materials Conference, April 22-25, Paper No. AIAA-2002-1444.
    • Shen, J., and Chopra, I., "Actuation Requirements for a Swashplateless Helicopter Control System with Trailing-Edge Flaps," Proc. of the 43rd AIAA/ASME/ASCE/ AHS /ASC Structures, Structural Dynamics, and Materials Conference, April 22-25, 2002, Paper No. AIAA-2002-1444.
    • (2002)
    • Shen, J.1    Chopra, I.2
  • 3
    • 84884345667 scopus 로고    scopus 로고
    • 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
    • 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.
    • (2002)
    • Shen, J.1    Chopra, I.2
  • 4
    • 4143083696 scopus 로고    scopus 로고
    • Helicopter Horizontal Tail Incidence Control to Reduce Rotor Cyclic Pitch and Blade Flapping
    • Proc. of the 60th Annual Forum of the American Helicopter Society, Baltimore, Maryland, June
    • Gandhi, F., and Sekula, M., "Helicopter Horizontal Tail Incidence Control to Reduce Rotor Cyclic Pitch and Blade Flapping," Proc. of the 60th Annual Forum of the American Helicopter Society, Baltimore, Maryland, June 2004
    • (2004)
    • Gandhi, F.1    Sekula, M.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.