To help prevent the problem of mass reduction late in a spacecraft development program, the process of estimating spacecraft mass has been formulated in algorithmic form and incorporated in software that will allow trained users to interface with the integral design parameters data base interactively. The software will use historical data to extrapolate future values of a given time-dependent parameter and be manipulated by a dynamic graphics configuration builder. Future expansions of this work promise to automate the entire conceptual mission design process.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Automating the process of estimating spacecraft mass


    Beteiligte:
    Skinner, D. L. (Autor:in)

    Kongress:

    Annual Conference of the Society of Allied Weight Engineers ; 1980 ; St. Louis, MO


    Erscheinungsdatum :

    1980-05-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Automating the Process of Optimization in Spacecraft Design

    Fukunaga, A. S. / Chien, S. / Mutz, D. et al. | British Library Conference Proceedings | 1997


    Towards Automating Spacecraft Attitude Sensor Calibration

    Sedlak, Joseph / Welter, Gary / Ottenstein, Neil | NTRS | 2003



    Automating Trend Analysis for Spacecraft Constellations

    Davis, George / Cooter, Miranda / Updike, Clark et al. | NTRS | 2001


    Automating Spacecraft Maneuver Planning and Execution

    Johnson, G.K. / Hoover, S.A. / Aparicio, A.J. | AIAA | 2004