Aircraft loss-of-control, in particular approach to stall or fully developed stall, is a major factor contributing to aircraft safety risks, which emphasizes the need to develop algorithms that are capable of assisting the pilots to identify the problem and providing guidance to recover the aircraft. In this paper we present several stall recovery guidance algorithms, which are implemented in the background without interfering with flight control system and altering the pilot's actions. They are using input and state constrained control methods to generate guidance signals, which are provided to the pilot in the form of visual cues. It is the pilot's decision to follow these signals. The algorithms are validated in the pilot-in-the loop medium fidelity simulation experiment.


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    Titel :

    Stall Recovery Guidance Algorithms Based on Constrained Control Approaches


    Beteiligte:
    Stepanyan V. (Autor:in) / Krishnakumar K. (Autor:in) / Kaneshige J. (Autor:in) / Acosta D. (Autor:in)

    Erscheinungsdatum :

    2016


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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