Previous analysis identified specific orbital parameters as being safer for conjunction avoidance for the TDRS fleet. With TDRS-9 being considered an at-risk spacecraft, a potential conjunction concern was raised should TDRS-9 fail while at a longitude of 12W. This document summarizes the analysis performed to identify if these specific orbital parameters could be targeted using the remaining drift-termination maneuvers for the relocation of TDRS-9 from 41W longitude to 12W longitude.


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    Title :

    Differential Evolution Optimization for Targeting Spacecraft Maneuver Plans


    Contributors:
    D. Mattern (author)

    Publication date :

    2016


    Size :

    31 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English