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Volumn , Issue , 2009, Pages

L1 adaptive control design for NASA AirSTAR flight test vehicle

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL THEORY; ENVIRONMENTAL REGULATIONS; NASA;

EID: 78049294790     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-5738     Document Type: Conference Paper
Times cited : (117)

References (25)
  • 1
    • 78651247100 scopus 로고    scopus 로고
    • Practical application of a subscale transport aircraft for flight research in control upset and failure conditions
    • AIAA 2008-6200, Honolulu, HI
    • Cunningham K., Foster J. V., Morelli E. A., and Murch A. M., "Practical Application of a Subscale Transport Aircraft for Flight Research in Control Upset and Failure Conditions," AIAA 2008-6200, AIAA Atmospheric Flight Mechanics Conference, Honolulu, HI, 2008.
    • (2008) AIAA Atmospheric Flight Mechanics Conference
    • Cunningham, K.1    Foster, J.V.2    Morelli, E.A.3    Murch, A.M.4
  • 2
    • 77957801831 scopus 로고    scopus 로고
    • A flight control system architecture for the NASA AirSTAR flight test infrastructure
    • AIAA 2008-6990, Honolulu, HI
    • Murch, A. M., "A Flight Control System Architecture for the NASA AirSTAR Flight Test Infrastructure," AIAA 2008-6990, AIAA Guidance, Navigation, and Control Conference and Exhibit, Honolulu, HI, 2008.
    • (2008) AIAA Guidance, Navigation, and Control Conference and Exhibit
    • Murch, A.M.1
  • 3
    • 77958501834 scopus 로고    scopus 로고
    • Software considerations for subscale flight testing of experimental control laws
    • To be presented at , Seattle, WA, April
    • Murch, A. M., Cox, D.E, Cunningham K.," Software Considerations for Subscale Flight Testing of Experimental Control Laws," To be presented at The InfoTech@Aerospace 2009, Seattle, WA, April, 2009.
    • (2009) The InfoTech@Aerospace 2009
    • Murch, A.M.1    Cox, D.E.2    Cunningham, K.3
  • 5
    • 29744446871 scopus 로고    scopus 로고
    • Airborne subscale transport aircraft research testbed - Aircraft model development
    • AIAA 2005-6432, San Francisco, CA
    • Jordan, T. L., Langford, W. M., and Hill, J. S., "Airborne Subscale Transport Aircraft Research Testbed - Aircraft Model Development," AIAA 2005-6432, AIAA Guidance, Navigation, and Control Conference, San Francisco, CA, 2005.
    • (2005) AIAA Guidance, Navigation, and Control Conference
    • Jordan, T.L.1    Langford, W.M.2    Hill, J.S.3
  • 8
    • 46149103938 scopus 로고    scopus 로고
    • 1 adaptive controller for systems with unknown time-varying parameters and disturbances in the presence of non-zero trajectory initialization error
    • 1 Adaptive Controller for Systems with Unknown Time-varying Parameters and Disturbances in the Presence of Non-zero Trajectory Initialization Error, International Journal of Control, vol. 81, No. 7, pp. 1148-1162, 2008.
    • (2008) International Journal of Control , vol.81 , Issue.7 , pp. 1148-1162
    • Cao, C.1    Hovakimyan, N.2
  • 9
    • 42649092134 scopus 로고    scopus 로고
    • 1 adaptive output feedback controller for systems of unknown dimension
    • 1 Adaptive Output Feedback Controller for Systems of Unknown Dimension, IEEE Transactions on Automatic Control, vol. 53, No. 3, pp. 815-821, 2008.
    • (2008) IEEE Transactions on Automatic Control , vol.53 , Issue.3 , pp. 815-821
    • Cao, C.1    Hovakimyan, N.2
  • 11
    • 46449123646 scopus 로고    scopus 로고
    • 1 adaptive controller for systems with unknown time-varying parameters and bounded disturbances.
    • 1 Adaptive Controller for Systems with Unknown Time-varying Parameters and Bounded Disturbances." American Control Conference, pp. 3925-3930, 2007.
    • (2007) American Control Conference , pp. 3925-3930
    • Cao, C.1    Hovakimyan, N.2
  • 17
    • 67149130101 scopus 로고    scopus 로고
    • 1 adaptive output-feedback controller for non-strictly-positive-real reference systems: Missile longitudinal autopilot design.
    • May-June
    • 1 Adaptive Output-Feedback Controller for Non-Strictly-Positive-Real Reference Systems: Missile Longitudinal Autopilot Design." Journal of Guidance, Control and Dynamics, vol. 32, no. 3, pp.717-726, May-June 2009.
    • (2009) Journal of Guidance, Control and Dynamics , vol.32 , Issue.3 , pp. 717-726
    • Cao ., C.1    Hovakimyan, N.2
  • 19
    • 77958182155 scopus 로고    scopus 로고
    • Aerodynamic effects and modeling of damage to transport aircraft
    • AIAA-2008-6203 , Honolulu, HI
    • Shah, G. "Aerodynamic Effects and Modeling of Damage to Transport Aircraft." AIAA-2008-6203 AIAA Guidance, Navigation, and Control Conference, Honolulu, HI, 2008.
    • (2008) AIAA Guidance, Navigation, and Control Conference
    • Shah, G.1
  • 21
    • 33845749151 scopus 로고    scopus 로고
    • Application and flight testing of an adaptive autopilot on precision guided munitions
    • AA-2006-6568, Keystone, CO, August
    • Sharma, M., E. Lavretsky, and K.A. Wise, "Application and Flight Testing of an Adaptive Autopilot on Precision Guided Munitions," AIAA-2006-6568, AIAA Guidance, Navigation, and Control Conference, Keystone, CO, August 2006.
    • (2006) AIAA Guidance, Navigation, and Control Conference
    • Sharma, M.1    Lavretsky, E.2    Wise, K.A.3
  • 23
    • 78650013079 scopus 로고    scopus 로고
    • 1 adaptive controller for nonlinear systems in the presence of significant cross-coupling
    • submitted to the , June, Baltimore, MD
    • Xargay, E., Hovakimyan, N. and C. Cao, "L1 Adaptive Controller for Nonlinear Systems in the Presence of Significant Cross-Coupling," submitted to the 2010 American Control Conference, June 2010, Baltimore, MD.
    • (2010) 2010 American Control Conference
    • Xargay, E.1    Hovakimyan, N.2    Cao, C.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.