A guidance algorithm that provides precise rendezvous in the deterministic case while requiring only relative state information is developed. A navigation scheme employing only onboard relative measurements is built around a Kalman filter set in measurement coordinates. The overall guidance and navigation procedure is evaluated in the face of measurement errors by a detailed numerical simulation. Results indicate that onboard guidance and navigation for the terminal phase of rendezvous is possible with reasonable limits on measurement errors.


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    Title :

    Solar electric propulsion for terminal flight to rendezvous with comets and asteroids


    Contributors:
    Bennett, A. (author)

    Conference:

    Electric Propulsion Conference ; 1973 ; Lake Tahoe, NV


    Publication date :

    1973-10-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :