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    Flight Test of L1 Adaptive Control Law: Offset Landings and Large Flight Envelope Modeling Work

    Flight Test of L1 Adaptive Control Law: Offset Landings and Large Flight Envelope Modeling Work


    This paper presents new results of a flight test of the L1 adaptive control architecture designed to directly compensate for significant uncertain cross-coupling in nonlinear systems. The flight test was conducted on the subscale turbine powered Generic Transport Model that is an integral part of the Airborne Subscale Transport Aircraft Research system at the NASA Langley Research Center. The results presented include control law evaluation for piloted offset landing tasks as well as results in support of nonlinear aerodynamic modeling and real-time dynamic modeling of the departure-prone edges of the flight envelope.

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    Titel :

    Flight Test of L1 Adaptive Control Law: Offset Landings and Large Flight Envelope Modeling Work

    Beteiligte:
    I. M. Gregory (Autor:in) / E. Xargay (Autor:in) / C. Cao (Autor:in) / N. Hovakimyan (Autor:in)
    Erscheinungsdatum :

    2011

    Format / Umfang :

    15 pages

    Medientyp :

    Report

    Format :

    Keine Angabe

    Sprache :

    Englisch

    Schlagwörter :

    Aircraft , Test Facilities & Equipment , Adaptive control , Cross coupling , Dynamic models , Transport aircraft , Flight tests , Nonlinear systems , Flight envelopes , Real time operation , Turbines , Control theory

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