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Volumn 1, Issue , 2004, Pages 282-297

Dynamic flight guidance recalibration after actuator failure

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRCRAFT; AIRCRAFT LANDING; APPROXIMATION THEORY; GLOBAL POSITIONING SYSTEM; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS;

EID: 19944380451     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-6255     Document Type: Conference Paper
Times cited : (22)

References (18)
  • 1
    • 0035438526 scopus 로고    scopus 로고
    • Development and evaluation of a cockpit decision aid for emergency trajectory generation
    • Sept.-Oct.
    • Chen, T. L. and Pritchett, A. R., "Development and Evaluation of a Cockpit Decision Aid for Emergency Trajectory Generation," AIAA Journal of Aircraft, Vol. 38, No. 5, Sept.-Oct. 2001, pp. 935-943.
    • (2001) AIAA Journal of Aircraft , vol.38 , Issue.5 , pp. 935-943
    • Chen, T.L.1    Pritchett, A.R.2
  • 3
    • 84896051321 scopus 로고    scopus 로고
    • An integrated fault management system for unmanned aerial vehicles
    • San Diego, CA, Sept., (AIAA2003-6642)
    • Boskovic, J. D. and Mehra, R. K., "An Integrated Fault Management System for Unmanned Aerial Vehicles," Proc. of the 2nd AIAA Unmanned Unlimited Conference, San Diego, CA, Sept. 2003, (AIAA2003-6642).
    • (2003) Proc. of the 2nd AIAA Unmanned Unlimited Conference
    • Boskovic, J.D.1    Mehra, R.K.2
  • 6
  • 15
  • 18
    • 85040158804 scopus 로고
    • Simulator study of stall/post-stall characteristics of a fighter airplane with relaxed longitudinal static stability
    • Washington, D.C., Dec.
    • Nguyen, L. T., "Simulator study of stall/post-stall characteristics of a fighter airplane with relaxed longitudinal static stability," Nasa tech. pap. 1538, Washington, D.C., Dec. 1979.
    • (1979) Nasa Tech. Pap. , vol.1538
    • Nguyen, L.T.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.