NASA is providing preliminary design and requirements for the Space Launch System Exploration Upper Stage (EUS). The EUS will provide upper stage capability for vehicle ascent as well as on-orbit control capability. Requirements include performance of on-orbit burn to provide Orion vehicle with escape velocity. On-orbit attitude control is accommodated by a on-off Reaction Control System (RCS). Paper provides overview of approaches for design and stability of an attitude control system using a RCS.


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    Titel :

    Design and Stability of an On-Orbit Attitude Control System Using Reaction Control Thrusters


    Beteiligte:
    Hall, Robert A. (Autor:in) / Hough, Steven (Autor:in) / Orphee, Carolina (Autor:in) / Clements, Keith (Autor:in)

    Kongress:

    AIAA SciTech 2016 ; 2016 ; San Diego, CA, United States
    AIAA Guidance, Navigation, and Control Conference ; 2016 ; San Diego, CA, United States


    Erscheinungsdatum :

    2016-01-04


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Design and Stability of an On-Orbit Attitude Control System Using Reaction Control Thrusters

    Hall, Robert A. / Hough, Steven / Orphee, Carolina et al. | AIAA | 2016



    Design and Stability of an On-Orbit Attitude Control System Using Reaction Control Thrusters

    Hall, Robert A. / Hough, Steven / Orphee, Carolina et al. | NTRS | 2015


    Design and Stability of an On-Orbit Attitude Control System Using Reaction Control Thrusters

    Hall, Robert A. / Hough, Steven / Orphee, Carolina et al. | NTRS | 2016