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Volumn 1, Issue , 2005, Pages 326-341

Nonlinear robust autoland

Author keywords

[No Author keywords available]

Indexed keywords

AUTOLAND DESIGN; FEEDBACK LINEARIZATION; OUTER LOOP; ROBUST MULTI-INVERSION (RMI);

EID: 29744433350     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (8)

References (26)
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  • 7
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  • 8
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    • Dynamic contraction method approach to robust longitudinal flight control under aircraft parameters variations
    • Austin. 11-14/08/2003
    • CZYBA Roman and BLACHUTA Marian J., "Dynamic contraction method approach to robust longitudinal flight control under aircraft parameters variations", AIAA guidance, navigation and control conference, Austin. 11-14/08/2003.
    • AIAA Guidance, Navigation and Control Conference
    • Czyba, R.1    Blachuta, M.J.2
  • 9
    • 0003096706 scopus 로고
    • Dynamic inversion: An evolving methodology for flight control design
    • ENNS Dale, BUGASKI Dan, HENDRICK Russ and STEIN Gunter, "Dynamic inversion: an evolving methodology for flight control design", Int. J. Control, Vol. 59, No. 1, 71-91, 1984.
    • (1984) Int. J. Control , vol.59 , Issue.1 , pp. 71-91
    • Enns, D.1    Bugaski, D.2    Hendrick, R.3    Stein, G.4
  • 16
    • 0024051348 scopus 로고
    • Flight control design using non-linear inverse dynamics
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  • 19
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    • AGARD AG-251
    • MEYER George and CICOLANI Luigi, "Application of nonlinear systems inverses to automatic flight control design - System concepts and flight evaluations", AGARD AG-251, Theory and applications of optimal control in aerospace systems, 1980.
    • (1980) Theory and Applications of Optimal Control in Aerospace Systems
    • Meyer, G.1    Cicolani, L.2
  • 20
    • 0029754194 scopus 로고    scopus 로고
    • Stability of dynamic inversion control laws applied to nonlinear aircraft pitch-axis models
    • MORTON Blaise, ENNS Dale and ZHANG Bing-Yu "Stability of dynamic inversion control laws applied to nonlinear aircraft pitch-axis models", Int. J. Control, Vol. 63, No. 1, 1-25, 1996.
    • (1996) Int. J. Control , vol.63 , Issue.1 , pp. 1-25
    • Morton, B.1    Enns, D.2    Zhang, B.-Y.3
  • 21
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    • Flight control design using robust dynamic inversion and time-scale separation
    • REINER Jacob, BALAS Gary J. and GARRARD William L., "Flight control design using robust dynamic inversion and time-scale separation", Automatica, Vol. 25, No. 11, Pp. 1493-1504, 1996.
    • (1996) Automatica , vol.25 , Issue.11 , pp. 1493-1504
    • Reiner, J.1    Balas, G.J.2    Garrard, W.L.3
  • 22
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    • Robust dynamic inversion for control of highly manoeuverable aircraft
    • January-february
    • REINER Jacob, BALAS Gary J. and GARRARD William L., "Robust dynamic inversion for control of highly manoeuverable aircraft", Journal of guidance, control and dynamics, Vol. 18, No.1, January-february 1995.
    • (1995) Journal of Guidance, Control and Dynamics , vol.18 , Issue.1
    • Reiner, J.1    Balas, G.J.2    Garrard, W.L.3
  • 23
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    • Septembre-october
    • SINGH Sahjendra N., STEINBERG Marc and DIGIROLAMO Robert D., "Nonlinear predictive control of feedback linearizable systems and flight control system design", Journal of guidance, control and dynamics, Vol. 18, No. 5, Septembre-october 1995.
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    • Singh, S.N.1    Steinberg, M.2    Digirolamo, R.D.3
  • 24
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    • July-august
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  • 26
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    • Comparison of intelligent, adaptive and nonlinear flight control laws
    • July-August
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    • (2001) Journal of Guidance, Control and Dynamics , vol.24 , Issue.4
    • Steinberg, M.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.