On October 23, 2015, the Dawn spacecraft left the High Altitude Mapping Orbit (HAMO) around Ceres and began its final decent to the Low Altitude Mapping Orbit (LAMO), arriving on December 15. The transfer between the two science orbits, a tight spiraling trajectory with over 100 revolutions, required the operations team to perform weekly maneuver designs for a period of 50 days. While the first six weeks of the transfer executed as planned, unexpectedly the spacecraft incurred a multi-sigma delivery error to the final science orbit that was subsequently clean-up at the first orbit maintenance maneuver. In this paper we discuss the design architecture for the transfer in detail, including challenges the team faced in flying the transfer and lessons learned.


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    Titel :

    Design and Execution of Dawn HAMO to LAMO Transfer at Ceres


    Beteiligte:

    Kongress:

    AIAA/AAS Astrodynamics Specialist Conference ; 2016 ; Long Beach, CA, United States


    Erscheinungsdatum :

    13.09.2016



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    DESIGN AND EXECUTION OF DAWN HAMO TO LAMO TRANSFER AT CERES

    Grebow, Daniel J. / Kennedy, Brian M. / Han, Dongsuk et al. | British Library Conference Proceedings | 2016


    Design and Execution of Dawn HAMO to LAMO Transfer at Ceres

    Grebow, Daniel / Kennedy, Brian / Han, Dongsuk et al. | AIAA | 2016



    IN-FLIGHT OPERATION OF THE DAWN ION PROPULSION SYSTEM THROUGH OPERATIONS IN THE LAMO ORBIT AT CERES (AIAA 2016-4539)

    Garner, Charles E. / Rayman, Marc D. | British Library Conference Proceedings | 2016