메뉴 건너뛰기




Volumn , Issue , 2014, Pages 1158-1166

Ground effect experiments and model validation with Draganflyer X8 rotorcraft

Author keywords

[No Author keywords available]

Indexed keywords

EXPERIMENTS; GROUND EFFECT; PROPELLERS; UNMANNED AERIAL VEHICLES (UAV); UNMANNED VEHICLES;

EID: 84904556682     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ICUAS.2014.6842370     Document Type: Conference Paper
Times cited : (60)

References (14)
  • 5
    • 0004245020 scopus 로고
    • Dover Publicatons Inc. New York
    • Wayne Johnson. Helicopter Theory. Dover Publicatons Inc., New York, 1980.
    • (1980) Helicopter Theory
    • Johnson, W.1
  • 6
    • 0033905356 scopus 로고    scopus 로고
    • Simulated flowfields in near-ground operation of single-and twin-rotor configurations
    • Ning Kang and Mao Sun. Simulated flowfields in near-ground operation of single-and twin-rotor configurations. Journal of Aircraft, 37(2):214-220, 2000.
    • (2000) Journal of Aircraft , vol.37 , Issue.2 , pp. 214-220
    • Kang, N.1    Sun, M.2
  • 7
    • 0012036669 scopus 로고
    • Analysis of ground effect on the lifting airscrew
    • National Advisory committee for Aeronautics
    • Montgomery Knight and Ralph A. Hegner. Analysis of ground effect on the lifting airscrew. Technical Report NACA-TN-835, National Advisory committee for Aeronautics, 1941.
    • (1941) Technical Report NACA-TN-835
    • Knight, M.1    Hegner, R.A.2
  • 9
    • 69949126532 scopus 로고    scopus 로고
    • Hover performance correlation for full-scale and model-scale coaxial rotors
    • Joon W. Lim, Kenneth W. McAlister, and Wayne Johnson. Hover performance correlation for full-scale and model-scale coaxial rotors. Journal of the American Helicopter Society, 54(3):1-14, 2009.
    • (2009) Journal of the American Helicopter Society , vol.54 , Issue.3 , pp. 1-14
    • Lim, J.W.1    McAlister, K.W.2    Johnson, W.3
  • 10
    • 80053137280 scopus 로고    scopus 로고
    • Integral sliding mode altitude control for a small model helicopter with ground effect compensation
    • San Francisco, CA, USA, June
    • Kenichiro Nonaka and Hirokazu Sugizaki. Integral sliding mode altitude control for a small model helicopter with ground effect compensation. In Proceedings of 2011 American Control Conference, pages 202-207, San Francisco, CA, USA, June 2011.
    • (2011) Proceedings of 2011 American Control Conference , pp. 202-207
    • Nonaka, K.1    Sugizaki, H.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.