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Volumn 356, Issue 1745, 1998, Pages 2203-2221

Piloted simulation tools for aircraft departure analysis

Author keywords

Bifurcation analysis; Combat aircraft; Departure prediction; Piloted simulation

Indexed keywords


EID: 3042894737     PISSN: 1364503X     EISSN: None     Source Type: Journal    
DOI: 10.1098/rsta.1998.0270     Document Type: Article
Times cited : (20)

References (15)
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    • Adams Jr., W.M.1
  • 2
    • 84983171465 scopus 로고    scopus 로고
    • Closed loop design for a simple non-linear aircraft model using eigenstructure assignment. AIAA-97-3779
    • New Orleans
    • Gibson, L., Nichols, N. K. & Littleboy, D. M. 1997 Closed loop design for a simple non-linear aircraft model using eigenstructure assignment. AIAA-97-3779, AIAA AFM Conference, New Orleans.
    • (1997) AIAA AFM Conference
    • Gibson, L.1    Nichols, N.K.2    Littleboy, D.M.3
  • 5
    • 85085847450 scopus 로고    scopus 로고
    • Maximum stability region design for unstable aircraft with control constraints. AIAA-96-3910
    • San Diego
    • Goman, M., Fedulova, E. & Khramtsovsky, A. 1996 Maximum stability region design for unstable aircraft with control constraints. AIAA-96-3910, AIAA AFM Conference, San Diego.
    • (1996) AIAA AFM Conference
    • Goman, M.1    Fedulova, E.2    Khramtsovsky, A.3
  • 6
    • 3042973808 scopus 로고
    • Bifurcation theory in flight dynamics: An application to a real combat aircraft
    • Guicheteau, P. 1990 Bifurcation theory in flight dynamics: an application to a real combat aircraft. ICAS Paper 116 (90-5.10.4).
    • (1990) ICAS Paper , vol.116
    • Guicheteau, P.1
  • 7
    • 0028195691 scopus 로고
    • Application of bifurcation theory to high-angle-of-attack dynamics of the F-14
    • Jahnke, C. C. & Culick, F. E. C. 1994 Application of bifurcation theory to high-angle-of-attack dynamics of the F-14. J. Aircraft 31, 26-34.
    • (1994) J. Aircraft , vol.31 , pp. 26-34
    • Jahnke, C.C.1    Culick, F.E.C.2
  • 8
    • 84982318243 scopus 로고    scopus 로고
    • Bifurcation analysis of a high incidence aircraft with non-linear dynamic inversion control. AIAA-97-3717
    • New Orleans
    • Littleboy, D. M. & Smith, P. R. 1997 Bifurcation analysis of a high incidence aircraft with non-linear dynamic inversion control. AIAA-97-3717, AIAA AFM Conference, New Orleans.
    • (1997) AIAA AFM Conference
    • Littleboy, D.M.1    Smith, P.R.2
  • 9
    • 84983140600 scopus 로고    scopus 로고
    • Stability and controllability evaluation of sustained flight manoeuvres. AIAA-96-3422
    • San Diego
    • Lowenberg, M. 1996 Stability and controllability evaluation of sustained flight manoeuvres. AIAA-96-3422, AIAA AFM Conference, San Diego, pp. 490-499.
    • (1996) AIAA AFM Conference , pp. 490-499
    • Lowenberg, M.1
  • 10
    • 0011713597 scopus 로고
    • Global stability and control analysis of aircraft at high angles-of attack
    • ONR-CR215-248-1. Scientific Systems Inc., USA
    • Mehra, R. D., Kessel, W. C. & Carroll, J. V. 1977 Global stability and control analysis of aircraft at high angles-of attack. Annual Technical Report 1, ONR-CR215-248-1. Scientific Systems Inc., USA.
    • (1977) Annual Technical Report 1
    • Mehra, R.D.1    Kessel, W.C.2    Carroll, J.V.3
  • 11
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    • Piloted simulation trial investigating departure characteristics of HIRM aircraft
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    • Patel, Y. 1996 Piloted simulation trial investigating departure characteristics of HIRM aircraft. DRA Customer Report, DRA/AS/FDS/CR96137/1.
    • (1996) DRA Customer Report
    • Patel, Y.1
  • 12
    • 84983197016 scopus 로고    scopus 로고
    • Departure analysis of a twin-finned, high performance combat aircraft. AIAA-96-3369-CP
    • San Diego
    • Patel, Y. & Smith, P. R. 1996 Departure analysis of a twin-finned, high performance combat aircraft. AIAA-96-3369-CP, AIAA AFM Conference, San Diego, pp. 80-87.
    • (1996) AIAA AFM Conference , pp. 80-87
    • Patel, Y.1    Smith, P.R.2
  • 14
    • 84997673901 scopus 로고
    • Functional control law design using exact non-linear dynamic inversion
    • Smith, P. R. 1994 Functional control law design using exact non-linear dynamic inversion. AIAA Atmospheric Flight Mechanics Conference, pp. 481-480.
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    • Smith, P.R.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.