Many large space system concepts will require active vibration control to satisfy critical performance requirements such as line-of-sight accuracy. In order for these concepts to become operational it is imperative that the benefits of active vibration control be practically demonstrated in ground based experiments. The results of the experiment successfully demonstrate active vibration control for a flexible structure. The testbed is the Active Control Technique Evaluation for Spacecraft (ACES) structure at NASA Marshall Space Flight Center. The ACES structure is dynamically traceable to future space systems and especially allows the study of line-of-sight control issues.


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    Title :

    Design and Implementation of Robust Decentralized Control Laws for the ACES Structure at Marshall Space Flight Center


    Contributors:

    Publication date :

    1990


    Size :

    76 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Design and implementation of robust decentralized control laws for the ACES structure at Marshall Space Flight Center

    Collins, Emmanuel G., Jr. / Phillips, Douglas J. / Hyland, David C. | NTRS | 1990


    Robust decentralized control laws for the ACES structure

    Collins, E.G. jun. / Phillips, D.J. / Hyland, D.C. | Tema Archive | 1991


    Marshall Space Flight Center Overview

    Geveden, Rex D. | NTRS | 2003