메뉴 건너뛰기




Volumn , Issue , 1997, Pages 1-11

An initial evaluation of the effects of motion platform and drive characteristics

Author keywords

[No Author keywords available]

Indexed keywords

CIRCUIT SIMULATION; SOFTWARE ENGINEERING;

EID: 84978209327     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (1)

References (14)
  • 3
    • 29244486762 scopus 로고
    • AGARD Advisory Report No. 144, AGARD, NATO, Neuilly sur Seine, France, September
    • Working Group: “Dynamic Characteristics of Flight Simulator Motion Systems,” AGARD Advisory Report No. 144, AGARD, NATO, Neuilly sur Seine, France, September 1979.
    • (1979) Dynamic Characteristics of Flight Simulator Motion Systems
  • 5
    • 84978183602 scopus 로고
    • U.S. Department of Transportation, Federal Aviation Administration, July
    • AC-120-40B, Airplane Simulator Qualification, U.S. Department of Transportation, Federal Aviation Administration, July 1991.
    • (1991)
  • 6
    • 84978232343 scopus 로고
    • U.S. Department of Transportation, Federal Aviation Administration, October
    • AC-120-63, Helicopter Simulator Qualification, U.S. Department of Transportation, Federal Aviation Administration, October 1994.
    • (1994)
  • 7
    • 0030713950 scopus 로고    scopus 로고
    • Visual and Roll- Lateral Motion Cueing Synchronization Requirements for Motion-Based Flight Simulations
    • April
    • Chung, W.Y. and Schroeder, J.A.: “Visual and Roll- Lateral Motion Cueing Synchronization Requirements for Motion-Based Flight Simulations,” American Helicopter Society’s 53rd Annual Forum, April 1997.
    • (1997) American Helicopter Society’s 53Rd Annual Forum
    • Chung, W.Y.1    Schroeder, J.A.2
  • 12
    • 0006453401 scopus 로고
    • The Use of Pilot Rating in the Evaluation of Aircraft Handling Qualities
    • Apr
    • Cooper, G. E.; and Harper, R. P Jr,: “The Use of Pilot Rating in the Evaluation of Aircraft Handling Qualities,” NASA TN D-5153, Apr. 1969.
    • (1969) NASA TN D-5153
    • Cooper, G.E.1    Harper, R.P.2
  • 13
    • 0026889693 scopus 로고
    • Frequency- Response Method for Rotorcraft System Identification: Flight Applications to BO-105 Coupled Rotor/Fuselage Dynamics
    • July
    • Tischler, M. B., Cauffman, M.G.: “Frequency- Response Method for Rotorcraft System Identification: Flight Applications to BO-105 Coupled Rotor/Fuselage Dynamics,” Journal of the American Helicopter Society, Vol 37, No 3, pgs 3-17, July 1992.
    • (1992) Journal of the American Helicopter Society , vol.37 , Issue.3 , pp. 3-17
    • Tischler, M.B.1    Cauffman, M.G.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.