Most Low Earth Orbit (LEO) spacecraft do not have thrusters and re-enter atmosphere in random locations at uncertain times. Objects pose a risk to persons, property, or other satellites. Has become a larger concern with the recent increase in small satellites. Working on a NASA funded project to design a retractable drag device to expedite de-orbit and target a re-entry location through modulation of the drag area. Will be discussing the re-entry point targeting algorithm here.


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    Titel :

    Re-Entry Point Targeting for LEO Spacecraft using Aerodynamic Drag


    Beteiligte:
    Omar, Sanny (Autor:in) / Bevilacqua, Riccardo (Autor:in) / Fineberg, Laurence (Autor:in) / Treptow, Justin (Autor:in) / Johnson, Yusef (Autor:in) / Clark, Scott (Autor:in)

    Kongress:

    Aerospace Control and Guidance Systems Committee Meeting ; 2016 ; Minneapolis, MN, United States


    Erscheinungsdatum :

    19.10.2016


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Omar, Sanny R. / Bevilacqua, Riccardo | NTRS | 2017



    Re-Entry Point Targeting for LEO Spacecraft using Aerodynamic Drag

    S. Omar / R. Bevilacqua / L. Fineberg et al. | NTIS | 2016



    Spacecraft Deorbit Point Targeting Using Aerodynamic Drag

    Omar, Sanny R. / Bevilacqua, Riccardo / Guglielmo, David et al. | AIAA | 2017

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