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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    Title :

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


    Contributors:
    R. A. Hall (author) / S. Hough (author) / C. Orphee (author) / K. Clements (author)

    Publication date :

    2016


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    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 | 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