메뉴 건너뛰기




Volumn , Issue , 2001, Pages

Structured adaptive model inversion applied to tracking aggressive aircraft maneuvers

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC STABILITY; AIRCRAFT; AIRCRAFT DETECTION; CLOSED LOOP SYSTEMS; EQUATIONS OF MOTION; ERRORS; NONLINEAR EQUATIONS;

EID: 85087599272     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-4019     Document Type: Conference Paper
Times cited : (22)

References (9)
  • 2
    • 0031268702 scopus 로고    scopus 로고
    • Adventures on the Interface of Dynamics and Control
    • Junkins, J. L., "Adventures on the Interface of Dynamics and Control," AIAA Journal of Guidance, Control and Dynamics, Vol. 20, No. 6, 1997, pp. 1058-1071.
    • (1997) AIAA Journal of Guidance, Control and Dynamics , vol.20 , Issue.6 , pp. 1058-1071
    • Junkins, J.L.1
  • 7
    • 0030194998 scopus 로고    scopus 로고
    • Adaptive Control of Feedback Linearizable Nonlinear Systems with Application to Flight Control
    • July-August
    • Singh, S. N. and Steinberg, M., "Adaptive Control of Feedback Linearizable Nonlinear Systems with Application to Flight Control," AIAA Journal of Guidance, Control and Dynamics, Vol. 19, No. 4, July-August, 1996, pp. 871-877.
    • (1996) AIAA Journal of Guidance, Control and Dynamics , vol.19 , Issue.4 , pp. 871-877
    • Singh, S.N.1    Steinberg, M.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.