The control of flexible spacecraft is a difficult problem because of large number of elastic modes; low value, closely-spaced frequencies; very small damping; and uncertainties in math models. The traditional design approach is to design the structure first and then to design the control system. This view-graph presentation develops a methodology for spacecraft design which addresses control/structure interaction issues, produces technology for simultaneous control/structure design, and translates into algorithms and computational tools for practical integrated computer-aided design.


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    Titel :

    Optimization-Based Approach for Integrated Controls-Structures Design of Flexible Spacecraft


    Beteiligte:
    P. G. Maghami (Autor:in) / S. M. Joshi (Autor:in) / E. S. Armstrong (Autor:in)

    Erscheinungsdatum :

    1994


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    An Optimization-Based Approach for Integrated Controls-Structures Design of Flexible Spacecraft

    Maghami, P. G. / Joshi, S. M. / Armstrong, E. S. et al. | British Library Conference Proceedings | 1994




    Integrated Controls-Structures Design Methodology for Flexible Spacecraft

    P. G. Maghami / S. M. Joshi / D. B. Price | NTIS | 1995


    Integrated Controls-Structures Design Methodology for Flexible Spacecraft

    Maghami, P. G. / Joshi, S. M. / Price, D. B. | NTRS | 1995