An adaptive augmenting control algorithm for the Space Launch System has been developed at the Marshall Space Flight Center as part of the launch vehicles baseline flight control system. A prototype version of the SLS flight control software was hosted on a piloted aircraft at the Armstrong Flight Research Center to demonstrate the adaptive controller on a full-scale realistic application in a relevant flight environment. Concerns regarding adverse interactions between the adaptive controller and a proposed manual steering mode were investigated by giving the pilot trajectory deviation cues and pitch rate command authority. Two NASA research pilots flew a total of twenty five constant pitch-rate trajectories using a prototype manual steering mode with and without adaptive control.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Launch Vehicle Manual Steering with Adaptive Augmenting Control In-flight Evaluations of Adverse Interactions Using a Piloted Aircraft


    Beteiligte:
    Hanson, Curt (Autor:in) / Miller, Chris (Autor:in) / Wall, John H. (Autor:in) / Vanzwieten, Tannen S. (Autor:in) / Gilligan, Eric (Autor:in) / Orr, Jeb S. (Autor:in)

    Kongress:

    SciTech 2015 ; 2015 ; Kissimmee, FL, United States


    Erscheinungsdatum :

    2015-01-08


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch