A systematic method for determining the optical placement of instrumentation on an arbitrary spacecraft is described. The method maximizes the resource utilization by minimizing the spacecraft's need for propulsive attitude control. The mathematical program developed with considerations toward reducing the size of the optimization effort is presented.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Optimization of payload placement on arbitrary spacecraft


    Contributors:


    Publication date :

    1991-10-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Optimization of payload placement on arbitrary spacecraft

    FEREBEE, MELVIN J. / ALLEN, CHERYL L. | AIAA | 1991


    SPACECRAFT PAYLOAD MODULE

    POKHABOV ALEKSANDR IUREVICH / BINDOKAS KIRILL ALGIRDASOVICH / SAVITSKII VIACHESLAV VASILEVICH et al. | European Patent Office | 2020

    Free access

    SPACECRAFT WITH EXTRA PAYLOAD

    ZHUL NIKOLAJ SERGEEVICH / SHAKLEIN PETR ALEKSEEVICH / JAKOVLEV ANDREJ VIKTOROVICH et al. | European Patent Office | 2016

    Free access

    Spacecraft payload ejection system

    SACHDEV TEJ SINGH / LYMER JOHN DOUGLAS / BRYAN RICHARD ANDREW et al. | European Patent Office | 2019

    Free access

    SPACECRAFT PAYLOAD MONITORING DEVICE

    SASAKI KO | European Patent Office | 2018

    Free access