메뉴 건너뛰기




Volumn 20, Issue 5, 1997, Pages 972-979

Analysis of adaptive neural networks for helicopter flight control

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; CONTROL SYSTEM ANALYSIS; DEGREES OF FREEDOM (MECHANICS); FLIGHT DYNAMICS; HELICOPTERS; MATHEMATICAL MODELS; MOTION CONTROL; NEURAL NETWORKS; ONLINE SYSTEMS;

EID: 0031237604     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4142     Document Type: Article
Times cited : (150)

References (11)
  • 1
    • 84976212589 scopus 로고
    • Design of a Helicopter Autopilot by Means of Linearizing Transformations
    • AGARD CP 321, also NASA TM-84295, A-9091, NAS 1.15;84295, Oct.
    • Meyer, G., Hunt, R. L., and Su, R., "Design of a Helicopter Autopilot by Means of Linearizing Transformations," Guidance and Control Panel, 35th Symposium, AGARD CP 321, 1983, pp. 4-1-4-11; also NASA TM-84295, A-9091, NAS 1.15;84295, Oct. 1982.
    • (1982) Guidance and Control Panel, 35th Symposium , pp. 41-411
    • Meyer, G.1    Hunt, R.L.2    Su, R.3
  • 2
    • 0018727650 scopus 로고
    • Total Aircraft Flight Control System-Balanced Open and Closed Loop Control with Dynamic Trim Maps
    • (Fort Worth, TX), Inst. of Electrical and Electronics Engineers, New York
    • Smith, G. A., and Meyer, G., "Total Aircraft Flight Control System-Balanced Open and Closed Loop Control with Dynamic Trim Maps," Challenge of the '80s; Proceedings of the Third Digital Avionics Systems Conference (Fort Worth, TX), Inst. of Electrical and Electronics Engineers, New York, 1979, pp. 215-223.
    • (1979) Challenge of the '80s; Proceedings of the Third Digital Avionics Systems Conference , pp. 215-223
    • Smith, G.A.1    Meyer, G.2
  • 4
  • 7
    • 0004178386 scopus 로고
    • Macmillan, New York
    • Khalil, H., Nonlinear Systems, Macmillan, New York, 1992, pp. 98-113.
    • (1992) Nonlinear Systems , pp. 98-113
    • Khalil, H.1
  • 9
    • 38249001473 scopus 로고
    • Synthesis of a Helicopter Nonlinear Controller Using Approximate Model Inversion
    • Prasad, J., and Lipp, A., "Synthesis of a Helicopter Nonlinear Controller Using Approximate Model Inversion," International Jounal on Mathematical and Computer Modeling, Vol. 18, No. 3/4, 1993, pp. 89-100.
    • (1993) International Jounal on Mathematical and Computer Modeling , vol.18 , Issue.3-4 , pp. 89-100
    • Prasad, J.1    Lipp, A.2
  • 10
    • 85081461973 scopus 로고
    • The Application of Flight Simulation Models in Support of Rotorcraft Design and Development
    • Shanthakumaran, P., "The Application of Flight Simulation Models in Support of Rotorcraft Design and Development," ACARD Conference Proceeding 513, 1991.
    • (1991) ACARD Conference Proceeding 513
    • Shanthakumaran, P.1
  • 11
    • 0028749528 scopus 로고
    • Helicopter Adaptive Flight Control Using Neural Networks
    • (Lake Buena Vista, FL), Inst of Electrical and Electronics Engineers, New York
    • Calise, A., Kim, B.-S., Leitner, J., and Prasad, J. V. R., "Helicopter Adaptive Flight Control Using Neural Networks," IEEE Conference on Decision and Control (Lake Buena Vista, FL), Inst of Electrical and Electronics Engineers, New York, 1994.
    • (1994) IEEE Conference on Decision and Control
    • Calise, A.1    Kim, B.-S.2    Leitner, J.3    Prasad, J.V.R.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.