메뉴 건너뛰기




Volumn 43, Issue 6, 2006, Pages 1914-1924

Effect of simulator motion on pilot behavior and perception

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE APPLICATIONS; BEHAVIORAL RESEARCH; MOTION COMPENSATION; MOTION PLANNING; SENSORY PERCEPTION;

EID: 33846037172     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.21900     Document Type: Article
Times cited : (36)

References (11)
  • 4
    • 33846120324 scopus 로고
    • Simulation Motion Effects on Single Axis Compensatory Tracking
    • AIAA Paper 93-3579, Aug
    • Schroeder, J.A., "Simulation Motion Effects on Single Axis Compensatory Tracking," AIAA Paper 93-3579, Aug. 1993.
    • (1993)
    • Schroeder, J.A.1
  • 5
    • 0030127050 scopus 로고    scopus 로고
    • Evaluation of Simulation Motion Fidelity Criteria in the Vertical and Directional Axes
    • April
    • Schroeder, J.A., "Evaluation of Simulation Motion Fidelity Criteria in the Vertical and Directional Axes," Journal of the American Helicopter Society, Vol. 41, No. 2, April 1996, pp. 44-57.
    • (1996) Journal of the American Helicopter Society , vol.41 , Issue.2 , pp. 44-57
    • Schroeder, J.A.1
  • 7
    • 29244449871 scopus 로고    scopus 로고
    • Pre and Post Pilot Model Analysis Compared to Experimental Simulator Results
    • AIAA Paper 2005-6303, Aug
    • Hosman, R.J.A.W., Grant, P.R., and Schroeder, J.A., "Pre and Post Pilot Model Analysis Compared to Experimental Simulator Results," AIAA Paper 2005-6303, Aug. 2005.
    • (2005)
    • Hosman, R.J.A.W.1    Grant, P.R.2    Schroeder, J.A.3
  • 8
    • 33846114851 scopus 로고
    • The Motion Characteristics of the UTIAS Motion System
    • UTIAS Tech. Note 261
    • Grant, P.R., "The Motion Characteristics of the UTIAS Motion System," UTIAS Tech. Note 261, 1986.
    • (1986)
    • Grant, P.R.1
  • 9
    • 4344706576 scopus 로고    scopus 로고
    • Empirically Derived Helicopter Response Model and Control System Requirements for Flight in Turbulence
    • July
    • Lusardi, J.A., Blanken, C.L., and Tischler, M.B., "Empirically Derived Helicopter Response Model and Control System Requirements for Flight in Turbulence," Journal of the American Helicopter Society, Vol. 49, No. 3, July 2004, pp. 340-349.
    • (2004) Journal of the American Helicopter Society , vol.49 , Issue.3 , pp. 340-349
    • Lusardi, J.A.1    Blanken, C.L.2    Tischler, M.B.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.