The enhanced attitude control system experiment is a technology demonstration experiment on the NASA's small spacecraft technology initiative program's Lewis spacecraft to evaluate advanced attitude control strategies. The purpose of the enhanced attitude control system experiment is to evaluate the feasibility of designing and implementing robust multi-input/multi-output attitude control strategies for enhanced pointing performance of spacecraft to improve the quality of the measurements of the science instruments. Different control design strategies based on modern and robust control theories are being considered for the enhanced attitude control system experiment. This paper describes the experiment as well as the design and synthesis of a mixed H(sub 2)/H(sub infinity) controller for attitude control. The control synthesis uses a nonlinear programming technique to tune the controller parameters and impose robustness and performance constraints. Simulations are carried out to demonstrate the feasibility of the proposed attitude control design strategy. Introduction


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Enhanced Attitude Control Experiment for SSTI Lewis Spacecraft


    Beteiligte:

    Erscheinungsdatum :

    01.01.1997


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch






    SSTI-Lewis Spacecraft Program

    Watkins, M. / Reppucci, G. | British Library Conference Proceedings | 1996


    SSTI-Lewis Spacecraft Nickel-Hydrogen Battery

    Tobias, R. F. / United States; National Aeronautics and Space Administration; Aerospace Flight Battery Systems Program | British Library Conference Proceedings | 1997