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Volumn 37, Issue 19, 2004, Pages 201-206

F16 icing identification based on neural networks

Author keywords

Aircraft control; Fault detection; Neural networks; Parameter identification

Indexed keywords

AIRCRAFT CONTROL; AIRCRAFT DETECTION; DEVELOPING COUNTRIES; FAULT DETECTION; IDENTIFICATION (CONTROL SYSTEMS); NEURAL NETWORKS; PARAMETER ESTIMATION; TRAINING AIRCRAFT;

EID: 84878302837     PISSN: 14746670     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1016/s1474-6670(17)30683-3     Document Type: Conference Paper
Times cited : (4)

References (18)
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    • Application of an improved LWR method to real-time aircraft parameter identification problems
    • Anchorage, AK, USA
    • Campa, G., Napolitano, M.R., Seanor, B., Fravolini, M.L., Song, Y. (2002). Application of an Improved LWR Method to Real-Time Aircraft Parameter Identification Problems, American Control Conference, Anchorage, AK, USA.
    • (2002) American Control Conference
    • Campa, G.1    Napolitano, M.R.2    Seanor, B.3    Fravolini, M.L.4    Song, Y.5
  • 9
    • 0035334816 scopus 로고    scopus 로고
    • Sensing aircraft icing effects by unsteady flap hinge- moment measurement
    • Gurbacki, H.M. and Bragg, M.B. (2001). Sensing Aircraft Icing Effects by Unsteady Flap Hinge- Moment Measurement, Journal of Aircraft, Vol. 39, No. 3, pp. 575-577.
    • (2001) Journal of Aircraft , vol.39 , Issue.3 , pp. 575-577
    • Gurbacki, H.M.1    Bragg, M.B.2
  • 11
    • 85088345052 scopus 로고    scopus 로고
    • Using artificial neural networks and self organizing maps for detection of airframe icing
    • AIAA-2000-4099
    • Johnson, M.D., Rokhsaz, K. (2000). Using Artificial Neural Networks And Self Organizing Maps for Detection of Airframe Icing, The 2000 Atmospheric Flight Mechanics Conference, AIAA-2000-4099.
    • (2000) The 2000 Atmospheric Flight Mechanics Conference
    • Johnson, M.D.1    Rokhsaz, K.2
  • 15
    • 0035678273 scopus 로고    scopus 로고
    • H-infinity parameter identification for in-flight detection of aircraft icing: The time varying case
    • Melody, J.W., Hillbrand, T., Baar, T., Perkins, W.R. (2001). H-Infinity Parameter Identification for In-flight Detection of Aircraft Icing: The Time Varying Case, IFAC Control Engineering Practice, 1327-1335.
    • (2001) IFAC Control Engineering Practice , pp. 1327-1335
    • Melody, J.W.1    Hillbrand, T.2    Baar, T.3    Perkins, W.R.4
  • 17
    • 29344458700 scopus 로고    scopus 로고
    • Detection of icing and related loss of control effectiveness in regional and corporate aircraft
    • AIAA-99-0637
    • Ribbens, W., Miller, R.H. (1999). Detection of Icing and Related Loss of Control Effectiveness in Regional and Corporate Aircraft, 37th Aerospace Sciences, AIAA-99-0637.
    • (1999) 37th Aerospace Sciences
    • Ribbens, W.1    Miller, R.H.2
  • 18
    • 19444381037 scopus 로고    scopus 로고
    • Characterizing the effect of ice on aircraft performance and control from flight data
    • Reno, NV, AIAA-2002-816
    • Whalen, E., Lee, S., Ratvasky, T. (2002). Characterizing the Effect of Ice on Aircraft Performance and Control From Flight Data, Aerospace Science Meeting and Exhibit, Reno, NV, AIAA-2002-816.
    • (2002) Aerospace Science Meeting and Exhibit
    • Whalen, E.1    Lee, S.2    Ratvasky, T.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.