메뉴 건너뛰기




Volumn , Issue , 1999, Pages 427-434

Ground effect modeling using a hybrid approach of inverse simulation and system identification

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC DRAG; AERODYNAMICS; FLIGHT SIMULATORS; INVERSE PROBLEMS; WAKES;

EID: 19644395537     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (8)

References (14)
  • 1
    • 84959189232 scopus 로고
    • Edition 1/26/95
    • FAA Airplane Simulator Qualification. Advisory Circular AC 120-40 C, Edition 1/26/95 (1995)
    • (1995) Advisory Circular AC 120-40 C
  • 7
    • 3743112357 scopus 로고
    • Aerospace vehicle modelling requirements for high bandwidth flight control. From
    • M.V. Cook and M. J. Rycraft, Clarendon Press, Oxford
    • P. G. Hamel Aerospace vehicle modelling requirements for high bandwidth flight control. From: "Aerospace Vehicle Dynamics and Control" by M.V. Cook and M. J. Rycraft, Clarendon Press, Oxford, pp. 1-31 (1994)
    • (1994) Aerospace Vehicle Dynamics and Control , pp. 1-31
    • Hamel, P.G.1
  • 8
    • 84959210091 scopus 로고
    • Ein 2-Punkt-Aerodynamikmodell fur die Identifizierung. Symposium
    • DFVLR-Mitt. 87-22, Paper Nr. 3.1
    • W. Monnich Ein 2-Punkt-Aerodynamikmodell fur die Identifizierung. Symposium 'Systemidenti-fizierung in der Fahrzeugdynamik', DFVLR-Mitt. 87-22, Paper Nr. 3.1 (1987)
    • (1987) Systemidenti-Fizierung in Der Fahrzeugdynamik
    • Monnich, W.1
  • 10
  • 12
    • 84959229507 scopus 로고
    • An Experimental Investigation into the Aerodynamic Characteristics of a Wing, with and without End Plates
    • P. E. Kumar An Experimental Investigation into the Aerodynamic Characteristics of a Wing, with and without End Plates, in Ground Effect. College of Aeronautics, Cranfield, Rep. No. 201 (1968)
    • (1968) Ground Effect. College of Aeronautics, Cranfield, Rep. No. 201
    • Kumar, P.E.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.