The results of the error analysis presented shows the feasibility of the proposed Apollo vehicle. The assumed accuracy of the optical vehicle-borne tracker of 0.0003 radians would produce sufficient accuracy to accomplish the mission without aid of earth based trackers during the midcourse and lunar phases of the flight. (Author)


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    Title :

    Guidance Error Analysis and Orbit Determination Accuracies for the Apollo Vehicle


    Contributors:
    P. Henry (author) / E. Dedman (author) / J. Hilton (author) / R. Seiley (author)

    Publication date :

    1961


    Size :

    50 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Orbit determination accuracies using satellite-to-satellite tracking

    Vonbun, F. O. / Argentiero, P. D. / Schmid, P. E. | NTRS | 1978


    Orbit determination accuracies using satellite-to-satellite tracking

    Vonbun, F. O. / Argentiero, P. D. / Schmid, P. E. | NTRS | 1978


    Orbit Determination Accuracies Using Satellite-to-Satellite Tracking

    Vonbun, F.O. / Argentiero, P.D. / Schmid, P.E. | IEEE | 1978


    Orbit determination accuracies using satellite-to-satellite tracking

    Vonbun, F.O. / Argentiero, P.D. / Schmid, P.E. | Tema Archive | 1978