Trajectory design of the orbit phase of the NEAR mission involves a new process that departs significantly from those procedures used in previous missions. In most cases, a precise spacecraft ephemeris is designed well in advance of arrival at the target body.


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    Title :

    Near Earth Asteroid Rendezvous (NEAR) Revised Eros Orbit Phase Trajectory Design


    Contributors:
    McADams, J. (author) / Farquhar, R. (author) / Dunham, D. (author) / Willimas, B. (author) / Carranza, E. (author) / Antreasian, P. (author) / Miller, J. (author) / Helfrich, C. (author)

    Publication date :

    1999-08-16


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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    Near Earth Asteroid Rendezvous orbit phase trajectory design

    Miller, J. / Carranza, E. / Helfrich, C. et al. | AIAA | 1998